Nuclear reactor control method and apparatus

ABSTRACT

A method for controlling a nuclear reactor is disclosed. The method includes providing a moderator zone in a core of the nuclear reactor, providing a fuel in the moderator zone, and providing one or more housings, each having a cavity, adjacent to the fuel. The method also includes allowing movement of a moderator between the moderator zone and the cavity of the one or more housings at a lower portion of the one or more housings. The method further includes confining moderator in the cavity of the one or more housings at an upper portion of the one or more housings.

RELATED APPLICATIONS

This is a continuing application of co-pending U.S. application Ser. No.13/468,467.

TECHNICAL FIELD

The present disclosure is directed to a nuclear reactor control methodand apparatus, and more particularly, to a control method and apparatusfor controlling a liquid moderated nuclear reactor.

BACKGROUND

Nuclear reactors using conventional reactor nuclear control systems haveseveral deficiencies. Reactors using conventional control systemsutilize constant adjustments to the quantity of neutron absorbingmaterial in the reactor core, and have a reduced conversion ratiobecause they absorb an excessive amount of neutrons. Also, reactorsusing conventional control systems do not have a relatively large rangeof reactivity control and thus use fuel with a relatively narrow rangeof fissile content. Further, reactors using conventional control systemsare frequently refueled, do not capture a large percentage of thepotential energy in fuel, and leave a relatively high amount ofradioactive waste per KWH of power generated.

The control method of the Canadian Deuterium Uranium reactors (CANDU)attempted to address some of these problems. However, the CANDU reactorused adjuster rods, which absorbed an excessive amount of neutrons, andthus did not provide a control system for adequately overcomingdeficiencies in conventional technology.

The present disclosure is directed to overcoming one or more of theshortcomings set forth above and/or other deficiencies in the art.

SUMMARY OF THE DISCLOSURE

In accordance with one aspect, the present disclosure is directed towarda method for controlling a nuclear reactor. The method includesproviding a moderator zone in a core of the nuclear reactor, providing afuel in the moderator zone, and providing one or more housings, eachhaving a cavity, adjacent to the fuel. The method also includes allowingmovement of a moderator between the moderator zone and the cavity of theone or more housings at a lower portion of the one or more housings. Themethod further includes confining moderator in the cavity of the one ormore housings at an upper portion of the one or more housings.

According to another aspect, the present disclosure is directed toward anuclear reactor core. The nuclear reactor core has a moderator zone, afuel disposed in the moderator zone, and one or more housings disposedadjacent to the fuel, each housing having a cavity. The lower portion ofeach housing is open for movement of the moderator between the moderatorzone and the cavity, and an upper portion of each housing is closed formovement of the moderator between the moderator zone and the cavity.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a schematic illustration of an exemplary disclosed nuclearreactor system;

FIG. 2 is a plan view of a first exemplary reactor of the nuclearreactor system of FIG. 1;

FIG. 2A is a plan scaled view of the arrangement of the nuclear reactorsystem of FIG. 1;

FIG. 3 is a sectional view taken through section A-A of the reactorshown in FIG. 2;

FIG. 3A is a scaled sectional view taken through section A-A of thereactor shown in FIG. 2;

FIG. 4 is a schematic illustration of an exemplary fuel tube arrangementof the reactor;

FIG. 5 is a side view of the fuel tube arrangement of FIG. 4;

FIG. 6 is a schematic illustration of another exemplary fuel tubearrangement of the reactor;

FIG. 7 is a sectional view taken through section B-B of the reactorshown in FIG. 3;

FIG. 8 is a detailed view of an exemplary control cavity array of thereactor;

FIG. 8A is another detailed view of an exemplary control cavity array ofthe reactor;

FIG. 8B is another detailed view of an exemplary control cavity array ofthe reactor;

FIG. 8C is a schematic illustration of an exemplary control cavity arrayof the reactor;

FIG. 8D is another schematic illustration of an exemplary control cavityarray of the reactor;

FIG. 9 is a sectional view of a second exemplary embodiment of thereactor;

FIG. 10 is a side view of the reactor of FIG. 9;

FIG. 11 is a detailed view of an exemplary control cavity array of thereactor of FIG. 9;

FIG. 12A is a plan view of a third exemplary embodiment of the reactor;

FIG. 12B is a sectional view of the third exemplary embodiment of thereactor;

FIG. 12C is a perspective view of the third exemplary embodiment of thereactor;

FIG. 12D is a schematic illustration of the third exemplary embodimentof the reactor;

FIG. 12E is another schematic illustration of the third exemplaryembodiment of the reactor;

FIG. 12F is another schematic illustration of the third exemplaryembodiment of the reactor;

FIG. 12G is another perspective view of the third exemplary embodimentof the reactor;

FIG. 12H is a plan view of a fourth exemplary embodiment of the reactor;

FIG. 12I is a sectional schematic view of the fourth exemplaryembodiment of the reactor;

FIG. 12J includes both a plan schematic view and a sectional schematicview of the fourth exemplary embodiment of the reactor;

FIG. 12K is a sectional schematic view of the fourth exemplaryembodiment of the reactor;

FIG. 12L includes both a schematic plan view and sectional schematicviews of the fourth exemplary embodiment of the reactor;

FIG. 12M includes both a schematic plan view and sectional schematicviews of the fourth exemplary embodiment of the reactor;

FIG. 12N includes a sectional schematic view of the fourth exemplaryembodiment of the reactor;

FIG. 13 is a schematic illustration of an exemplary reactor coolantsubsystem;

FIG. 14 is a sectional view of an exemplary passageway of the reactorcoolant subsystem;

FIG. 15 is a sectional view taken through section C-C of the reactorcontrol subsystem shown in FIG. 20;

FIG. 16 is a schematic illustration of a first exemplary auxiliarycoolant subsystem;

FIG. 17 is a schematic illustration of a second exemplary auxiliarycoolant subsystem;

FIG. 18 is a plan view of the second auxiliary coolant subsystem of FIG.17;

FIG. 19 is a schematic illustration of a third exemplary auxiliarycoolant subsystem; and

FIG. 20 is a schematic illustration of an exemplary reactor controlsubsystem.

DETAILED DESCRIPTION

FIG. 1 illustrates an exemplary nuclear reactor system 5 for generatingpower from a nuclear reaction. Nuclear reactor system 5 may include apower generation subsystem 10 and a reactor 15. Reactor 15 may provideenergy from a nuclear reaction to power generation subsystem 10. Nuclearreactor system 5 may also include a heat exchanger 20, a reactor coolantsubsystem 25, and a pump subsystem 30. Reactor coolant subsystem 25 mayfacilitate heat exchange between reactor 15 and heat exchanger 20, andpump subsystem 30 may pressurize reactor coolant subsystem 25. Nuclearreactor system 5 may further include an auxiliary coolant subsystem 35and a reactor control subsystem 40. Auxiliary coolant subsystem 35 mayprovide for additional heat transfer from reactor 15, and reactorcontrol subsystem 40 may control an operation of reactor 15.

Power generation subsystem 10 may include one or more turbines 45, oneor more drive assemblies 50, one or more generators 55, a turbinecooling subsystem 60, and a turbine steam subsystem 65. Turbine 45 maydrive generator 55 via drive assembly 50. Turbine steam subsystem 65 maytransfer water (H₂O) and steam (H₂O) between turbine 45 and turbinecooling subsystem 60. Turbine 45 may be any type of turbine that issuitable for use with a nuclear reactor such as, for example, a steamturbine. Turbine 45 may convert high pressure steam (H₂O) that isdelivered by turbine steam subsystem 65 into mechanical energy. Forexample, turbine 45 may include a plurality of elements mounted on arotatable shaft. The high pressure steam (H₂O) may enter turbine 45 andpass over the elements mounted on the shaft, the kinetic energy of thesteam (H₂O) thereby forcing the plurality of elements to rotate therotatable shaft. Turbine 45 may include a series of one or more highpressure cylinders followed by one or more low pressure cylinders. Eachcylinder may admit steam (H₂O) at a central portion, and the steam (H₂O)may progressively expand through the series of cylinders, thereby movingthe elements mounted on the shaft of turbine 45. Turbine 45 may includestationary elements that direct a steam (H₂O) flow within turbine 45.Turbine 45 may include additional systems such as, for example, ahydraulic control valve system having oil-operated valves to regulatesteam (H₂O) flow, a lubricating system for lubricating bearings thatsupport the cylinders, and a moisture separator for removing moisturefrom steam (H₂O) after leaving the high pressure cylinders and beforeentering the low pressure cylinders.

Drive assembly 50 may be any suitable assembly for transferringmechanical energy from turbine 45 to generator 55 such as, for example,a mechanical driveshaft assembly. Drive assembly 50 may operably connecta rotatable shaft of turbine 45 to generator 55 so that the kineticenergy from the steam (H₂O) hitting the elements mounted on the shaft ofturbine 45 may be transferred as mechanical energy to generator 55 viadrive assembly 50.

Generator 55 may be any type of generator that is suitable for use witha nuclear reactor such as, for example, an electrical generator. Forexample, generator 55 may include a magnet and wire arrangement forgenerating electricity from the mechanical energy transferred by driveassembly 50. For example, drive assembly 50 may rotate a magneticelement within generator 55 to generate electrical power. Generator 55may produce AC electricity at any suitable frequency such as, forexample, 50 Hz (50 cycle) or 60 Hz (60 cycle) power. Power generationsubsystem 10 may be operated to maintain one or more generators 55 at asubstantially constant frequency such as, for example, 50 or 60 cyclepower.

Turbine cooling subsystem 60 may be any type of cooling system that issuitable for use with a nuclear reactor such as, for example, a coolingsystem using condensers, cooling towers, and/or forced airflow for heatexchange. Turbine cooling subsystem 60 may remove surplus steam (H₂O)from turbine 45 and condense the surplus steam (H₂O) into water (H₂O).In addition to using condensers, cooling towers, and/or forced airflowto condense steam (H₂O) into water (H₂O), turbine cooling subsystem 60may also utilize nearby bodies of water (H₂O), if available andsuitable, for, e.g., once-through cooling.

Turbine steam subsystem 65 may be any type of arrangement suitable fortransferring water (H₂O) and steam (H₂O) between heat exchanger 20,turbine 45, and turbine cooling subsystem 60. Turbine steam subsystem 65may include a passageway 70 that transfers hot steam (H₂O) from heatexchanger 20 to turbine 45, a passageway 75 that transfers surplus ordead steam (H₂O) from turbine 45 to turbine cooling subsystem 60, and apassageway 80 that transfers relatively cold water (H₂O) from turbinecooling subsystem 60 to heat exchanger 20. Passageways 70, 75, and 80may be any suitable passageways for transferring steam (H₂O) and water(H₂O) such as, for example, steel pipe.

Nuclear reactor system 5 may also provide steam (H₂O) for any othersuitable purpose for which steam (H₂O) may be useful, in addition toproviding steam (H₂O) to turbines for power generation. For example,nuclear reactor system 5 may include configurations in which steam (H₂O)is not returned to the system after use, and/or in which input water(H₂O) comes from a source that is different from turbine steam subsystem65. For example, nuclear reactor system 5 may provide steam (H₂O) foruse in geothermal oil extraction.

Heat exchanger 20 may be any type of heat exchanger suitable fortransferring thermal energy between power generation subsystem 10 andreactor 15. For example, heat exchanger 20 may include one or more steamgenerators having a plurality of tubes through which hot reactor coolantof reactor coolant subsystem 25 flows. Each steam generator may include,for example, thousands of tubes for receiving hot reactor coolant. Forexample, each steam generator may include between about 3,000 and about16,000 tubes. The hot reactor coolant flowing through the steamgenerator tubes may boil water (H₂O) delivered to heat exchanger 20 byturbine steam subsystem 65. The steam (H₂O) generated by the steamgenerators of heat exchanger 20 may then be transferred to turbine 45via turbine steam subsystem 65. While passing through heat exchanger 20,reactor coolant may be cooled and may subsequently be returned toreactor 15 via reactor coolant subsystem 25.

Water (H₂O) delivered to heat exchanger 20 by turbine steam subsystem 65may enter heat exchanger 20 at an upper portion of heat exchanger 20.The relatively cold water (H₂O) may be injected into an interior portionof heat exchanger 20 via a plurality of nozzles 83 (see FIG. 20) thatmay be disposed at a central and/or upper portion of heat exchanger 20,on interior walls of heat exchanger 20. The plurality of nozzles 83 maybe oriented downward and may inject the water (H₂O) into boiling water(H₂O) already contained within heat exchanger 20. Therefore, therelatively cold water (H₂O) may be mixed with the boiling water (H₂O)already contained in heat exchanger 20, thereby helping to reduce amagnitude of a temperature gradient of H₂O contained inside heatexchanger 20. Heat exchanger 20 may thereby be able to produce steam(H₂O) at higher temperatures, due to the lower temperature gradient. Itis contemplated that the magnitude of the temperature gradient may alsobe further reduced by using a recirculation pump or by using acombination of convection currents, with entrainment of boiling water(H₂O) into the downward streams of relatively cold water (H₂O) fromnozzles 83.

Reactor 15 may be any type of nuclear reactor suitable for generatingpower from a nuclear reaction. Reactor 15 may be, for example, anynuclear reactor that uses liquid moderator. Also, for example, reactor15 may be a heavy water moderated and/or heavy water cooled reactor.Reactor 15 may be, for example, a CANDU reactor. As illustrated in FIG.2, reactor 15 may include a containment structure 85, a pressure vessel90, a reflector zone 95, and a reactor core 100. Containment structure85 and pressure vessel 90 may house reflector zone 95. Reactor core 100may be disposed in reflector zone 95.

Containment structure 85 may be any type of structure suitable forhousing reflector zone 95 and reactor core 100, and for shielding theenvironment outside of reactor 15 from radiation and neutrons emitted byreactor 15. For example, containment structure 85 may include reinforcedconcrete or prestressed concrete walls that surround reflector zone 95and reactor core 100. Containment structure 85 may have walls having anysuitable thickness for housing reflector zone 95 and reactor core 100such as, for example, between about four feet and about ten feet.Containment structure 85 may include apertures for receiving variouselements of reactor coolant subsystem 25, auxiliary coolant subsystem35, or other elements of nuclear reactor system 5. Containment structure85 may structurally support, insulate, and serve as a radiation barrierfor reflector zone 95 and reactor core 100. A reflecting pool may, forexample, simply fill the bottom of pressure vessel 90, or may beenclosed in separate containers as described further below.

Pressure vessel 90 may be any type of pressure vessel or structuresuitable for pressurizing reflector zone 95 and reactor core 100. Forexample, pressure vessel 90 may be a steel vessel that seals andpressurizes reflector zone 95 and reactor core 100. Pressure vessel 90may include one or more steel elements that are configured and/orconnected to form a sealed vessel. Pressure vessel 90 may include anyother suitable material with appropriate properties for use as apressure vessel such as, for example, materials having resistance tofracture and embrittlement. Pressure vessel 90 may be used whenreflector zone 95 and reactor core 100 include a “hot moderator” that ismaintained at a relatively high temperature. Pressure vessel 90 mayinclude apertures for receiving various elements of reactor coolantsubsystem 25, auxiliary coolant subsystem 35, or other elements ofnuclear reactor system 5. The apertures of pressure vessel 90 may besealed to maintain a pressurization of reflector zone 95 and reactorcore 100 within pressure vessel 90.

As illustrated in FIG. 3, reflector zone 95 may include a reflectingpool 105 and a steam area 110. A boundary 115 may separate reflectingpool 105 and steam area 110.

Reflecting pool 105 may include a moderator in a liquid state. Forexample, reflecting pool 105 may include D₂O (“heavy water”) in a liquidstate. Reflecting pool 105 may include D₂O manufactured to have anysuitable properties for moderating a nuclear reaction. For example, theD₂O of reflecting pool 105 may be reactor grade heavy water (99.75%pure). Reflecting pool 105 may also include H₂O (“light water”)moderator in a liquid state. Reflecting pool 105 may include a “hotmoderator” (e.g., FIG. 2) or a “cold moderator” (e.g., FIG. 11).

Steam area 110 may include a moderator that is of the same material asreflecting pool 105. Steam area 110 may include moderator that is in agaseous state. Heat from reactor core 100 may heat the moderator inreflector zone 95, causing some of the moderator to be held in a gaseousstate in steam area 110. The temperature of the gaseous moderator ofsteam area 110 is about the same as a temperature of the liquidmoderator of reflecting pool 105. Steam area 110 may fill substantiallythe entire reflector zone 95 if substantially all of the moderator isheated to a gaseous state. Also, reflecting pool 105 may fillsubstantially the entire the entire reflector zone 95 if substantiallyall of the moderator is cooled to a liquid state. A boundary 115 mayseparate reflecting pool 105 and steam area 110.

Four exemplary embodiments of a reactor core are disclosed below:reactor core 100, reactor core 100′, reactor core 100 a, and reactorcore 100 b. Wherever suitable, the various disclosed features of eachexemplary embodiment (for example, the reference numerals having an “a”modifier for reactor core 100 a) may be combined with features of theother embodiments. As disclosed further below, the disclosed exemplaryembodiments illustrate the wide range of possible embodiments of thedisclosed nuclear reactor system. For example, reactor core 100, 100′,100 a, and 100 b show that the disclosed nuclear reactor system mayinclude both vertical and horizontal fuel tube arrangements, both hotand cold moderator in the reactor core, different nuclear fuels such asuranium, plutonium, and thorium in different compositions such as metal,oxide, or salts, different fuel tube arrangements such as hexagonal andsquare arrangements, different types of moderator (e.g., D₂O and H₂O),different primary coolants (e.g. liquids such as D₂O, H₂O, and organicfluids; molten metals such as sodium and lead; molten salts, and gassessuch as helium) and different moderator cooling techniques (e.g., heatexchange and direct fluid exchange). By considering the exemplaryembodiments disclosed below, one of ordinary skill in the art wouldunderstand that the various disclosed features of each exemplaryembodiment may be combined with features of any other exemplaryembodiment, wherever appropriate.

As the first exemplary embodiment of the reactor core, reactor core 100may include a fuel assembly 125 and a control cavity array 130. Controlcavity array 130 may contain one or more pockets of moderator and/ormoderator steam adjacent to fuel assembly 125. Fuel tubes 135 may beoriented vertically in a square array with truncated corners (asillustrated in FIG. 4), and the moderator and fuel coolant may be heavywater (e.g., D₂O). The moderator may be cooled by conduction from aportion of the primary coolant (fuel coolant) flow.

Fuel assembly 125 may be any type of nuclear fuel suitable for use in anuclear reaction. For example, fuel assembly 125 may include bundles offuel rods that are disposed in a plurality of fuel tubes 135. Forexample, fuel assembly 125 may include an arrangement of hundreds offuel tubes 135. For example, fuel assembly 125 may include between about100 and about 500 fuel tubes 135 that may be about four inches indiameter. Each fuel tube 135 may include any suitable number of fuelbundles such as, for example, 12 fuel bundles. Each fuel bundle mayinclude any suitable number of fuel rods such as, for example, 37 fuelrods. Fuel assembly 125 may include any suitable fuel for a nuclearreaction such as, for example, natural uranium, enriched uranium, mixedoxide fuel (MOX), plutonium, thorium, and/or various mixtures of theseand other materials. For example, fuel assembly 125 may include a mixeduranium/plutonium fuel or a mixed uranium/thorium fuel.

Fuel assembly 125 may include fuel tubes 135 that are verticallydisposed (e.g., as illustrated in FIG. 2). Fuel assembly 125 may includefuel tubes 135 arranged in any suitable configuration such as, forexample, a right angle array as illustrated in FIGS. 4 and 5.

Referring back to FIG. 2, control cavity array 130 may include athree-dimensional array of control cavities 140. For example, thethree-dimensional array of control cavities 140 may serve as a housingto confine moderator adjacent to fuel tubes 135 of fuel assembly 125. Asdepicted in FIGS. 2, 3, and 7, the plurality of control cavities 140 maybe disposed horizontally to each other, as well as being stackedvertically. Control cavities 140 may be staggered vertically and/orhorizontally within control cavity array 130. For example, verticalstaggering of control cavities 140 is depicted in FIG. 3. Controlcavities 140 may be arranged in any suitable configuration for confininga moderator adjacent to fuel tubes 135.

FIGS. 2A and 3A illustrate different views of the arrangements ofreactor 15. FIG. 2A and FIG. 3A provide views of exemplary scaledarrangements of reactor 15.

As depicted in FIGS. 2 and 8, each control cavity 140 may include astructural assembly 145 and a cone assembly 150. Cone assembly 150 mayconfine moderator within structural assembly 145. Structural assembly145 may serve as a housing to confine moderator.

As depicted in FIGS. 2, 3, and 7, structural assembly 145 may includeone or more upper members 155, one or more side members 160, one or moreend members 165, and one or more intermediate members 170. Upper member155, side members 160, end member 165, and intermediate member 170 maybe formed from any suitable structural materials for confining moderatorsuch as, for example, zirconium alloy. Upper member 155, side members160, end member 165, and intermediate member 170 may be attached to eachother by any suitable technique such as, for example, welding. Uppermember 155, side members 160, end member 165, and intermediate member170 may also be integrally formed with each other. Upper member 155,side members 160, end member 165, and intermediate member 170 may be anysuitable structural member for confining moderator such as, for example,substantially flat and/or plate-like members. Upper member 155 may be,for example, a flat member disposed substantially horizontally at anupper portion of control cavity 140, and may be attached tosubstantially flat side members 160. End members 165 may be attached toend portions of upper member 155 and side members 160. Upper member 155,side members 160, and end members 165 may be attached to form, forexample, a cavity having a closed upper portion and an open bottomportion. Thus, upper member 155, side members 160, and end members 165may substantially prevent moderator movement in and out of an upperportion of control cavity 140, while allowing moderator to move in andout of a lower portion of control cavity 140. The upper portion ofcontrol cavity 140 may include upper member 155, upper portions of sidemembers 160, and upper portions of end members 165. The lower portion ofcontrol cavity 140 may include lower portions of side members 160 andlower portions of end members 165.

One or more intermediate members 170 may be disposed between andattached to side members 160 and upper member 155. Intermediate members170 may be disposed at any interval along control cavity 140.Intermediate members 170 may substantially prevent movement of moderatorthrough control cavity 140 at an upper portion of control cavity 140.End members 165 and intermediate members 170 may have a height that isless than a height of side members 160. Side members 160 of a givencontrol cavity 140 may be attached to upper member 155 of anothercontrol cavity 140 disposed below, for example, in the case that controlcavities 140 are vertically stacked. Because the height of end members165 and intermediate members 170 may be less than the height of sidemembers 160, moderator may be free to move under end members 165 andintermediate members 170 via gaps 175 and gaps 180, respectively, asdepicted in FIG. 7. Thus, end members 165 and intermediate members 170may serve as baffles to block movement of moderator in an upper portionof control cavity 140 and allow movement of moderator in a lower portionof control cavity 140. Gaps 180 may allow movement of moderator througha lower portion of control cavity 140, and gaps 175 may allow movementof moderator between reflector zone 95 and control cavity 140. Moderatormay not move under side members 160, which may be attached to uppermember 155 of the control cavity 140 disposed below. However, it alsocontemplated that gaps may be provided between side members 160 and theupper member 155 of control cavity 140 disposed below, to also allowmovement of moderator under some or all of side members 160. Thus, it isalso contemplated that moderator may be free to move between reflectorzone 95 and control cavities 140, under side members 160.

As depicted in FIGS. 3 and 7, control cavities 140 may include the samemoderator as reflector zone 95, because moderator may be free to movebetween reflector zone 95 and control cavities 140 via gaps 175 and 180.As moderator confined in control cavity 140 is heated by neutrons, gammaradiation, and/or thermal conduction from fuel tubes 135, some or all ofthe moderator in control cavity 140 may be heated into a gaseous statein a gaseous zone 185. Some or all of the moderator in control cavity140 may also be in a liquid state in a liquid zone 190. Gaseous zone 185and liquid zone 190 may be separated by a boundary 195. The size ofgaseous zone 185 and liquid zone 190 may vary between control cavities140, and between different intermediate members 170 within a singlecontrol cavity 140. Thus, the location of boundary 195 may vary betweencontrol cavities 140 and between different intermediate members 170within a single control cavity 140. For example, a given control cavity140 may have both a gaseous zone 185 and a liquid zone 190,substantially only a gaseous zone 185, or substantially only a liquidzone 190.

Heat imparted via neutrons, gamma radiation, and/or conduction from fueltubes 135 may cause the liquid moderator of liquid zone 190 to bemaintained at a temperature at or just below the boiling point of themoderator. For example, the moderator of liquid zone 190 may bemaintained in a simmering state. As the moderator in liquid zone 190simmers, some moderator may evaporate and rise into gaseous zone 185.Also, moderator in gaseous zone 185 that is near components of reactorcoolant subsystem 25 (e.g., as described below) may condense and dripback to liquid zone 190 along inner surfaces of control cavity 140. Thesize of gaseous zone 185 may therefore remain substantially constant,and boundary 195 may remain relatively stationary, when the amount ofheat imparted by fuel tubes 135 and the amount of heat removed byreactor coolant subsystem 25 are substantially equal. As describedfurther below, the size of gaseous zone 185 and a position of boundary195 may vary slightly over short periods of time (e.g., over a period ofdays) based on xenon and samarium absorption of neutrons, and may varysignificantly over long periods of time (e.g., over a period of years),based on, for example, an age (e.g., burnout) of the fuel. The size ofgaseous zone 185 and the position of boundary 195 may vary slightlyduring and shortly after periods of change in the rate of cooling byreactor coolant subsystem 25.

As depicted in greater detail in FIG. 8, cone assembly 150 may includean inner cone assembly 200, an outer cone assembly 205, and a passageway210. Cone assemblies 150 may provide a structural interface between fueltubes 135, which may pass through control cavities 140, and may help tomore evenly distribute heat from fuel tubes 135 within control cavities140. Inner cone assembly 200 may encircle a portion of fuel tube 135,outer cone assembly 205 may encircle inner cone assembly 200, andpassageway 210 may be disposed between inner cone assembly 200 and outercone assembly 205.

Inner cone assembly 200 may include a cone 215 that may encircle aportion of fuel tube 135. Cone 215 may be formed from any suitablematerial for confining liquid moderator or steam moderator withincontrol cavity 140 such as, for example, zirconium alloy. Cone 215 maybe formed from separate elements or may be integrally formed as a singleelement. Cone 215 may also have any suitable height for confiningmoderator. For example, cone 215 may have a height that is about twicethe height of control cavity 140. Cone 215 may pass through an aperturethat is formed in upper member 155 of structural assembly 145. Cone 215may be disposed at each control cavity 140. Because cone 215 may have aheight that is greater than a height of control cavity 140, cone 215 mayoverlap with other cones 215 encircling the same fuel tube 135. Cone 215may form a passageway 220 with fuel tube 135, and overlapping cones 215may form a passageway 225 between each other. Passageway 220 may be acontinuation of passageway 225. Passageways 220 and 225 may encirclefuel tubes 135, and may be any suitable shape such as, for example,conical-shaped passageways. Cone 215 may be sealed to fuel tube 135 atthe top of cone 215 so that passageway 220 may be a dead end, withpassageway 220 being sealed at the top. Because fuel tube 135 mayusually be hotter than the boiling point of the moderator, any moderatorin passageway 220 may boil and the resulting steam moderator will forcethe liquid moderator down out of the bottom of passageways 220 and 225via a gap 250 and into the lower portion of control cavity 140. Becausesteam may conduct heat less effectively than liquid moderator, theresulting double steam gap formed by passageways 220 and 225 and theoverlapping cones 215 may reduce the transfer of heat from fuel tubes135 to the moderator in control cavity 140. Thus, cones 215 mayeffectively encircle fuel tubes 135 with a thin layer of steam moderatorin passageways 220 and 225, the steam moderator being in fluidcommunication with reflector zone 95.

Outer cone assembly 205 may include an interior cone 235 and an exteriorcone 240. Interior cone 235 and exterior cone 240 may be of a materialsimilar to cone 215, and may encircle fuel tube 135 and cone 215.Interior cone 235 may be attached to a bottom surface 245 of uppermember 155 and may be intermittently attached at the bottom of interiorcone 235 to the bottom of cone 215 for structural integrity, while stillleaving a gap 230 that may allow vertical flow of liquid moderator fromthe lower portion of a cavity 140 via passageway 210 to cavities 140above and below. Interior cone 235 may have a height that is slightlyless than a height of control cavity 140, and may form gap 250 with anupper surface 255 of an adjacent control cavity 140 that is disposedbelow. Exterior cone 240 may also be attached to bottom surface 245 ofupper member 155, and may have a height that is less than a height ofinterior cone 235. A cavity 260 may be formed between interior cone 235and exterior cone 240. Moderator may be free to move between liquid zone190 of control cavity 140 and cavity 260. Moderator may also be free tomove between liquid zone 190 and a portion 270 disposed between adjacentexterior cones 240 of adjacent fuel tubes 135. A liquid zone 275including liquid moderator may be disposed in cavity 260. As fastneutrons and gamma radiation from fuel tubes 135 heat the moderator incontrol cavity 140, liquid moderator in liquid zone 275 may be heatedinto steam moderator and may form a gaseous zone 280. Also, as higherspeed (e.g., fast) neutrons and gamma radiation from fuel tubes 135 heatthe moderator in control cavity 140, liquid moderator in liquid zone 190may be heated into steam moderator and may form a portion of gaseouszone 185 within portion 270 disposed between adjacent exterior cones240. Depending on the amount of heat imparted by higher speed (e.g.,fast) neutrons and gamma radiation from fuel tubes 135, cavity 260 andportion 270 may be substantially entirely filled by gaseous zone 280 and185, respectively, or may be substantially entirely filled by liquidzones 275 and 190, respectively.

A boundary 290 may separate liquid zone 275 and gaseous zone 280, andboundary 195 may separate liquid zone 190 and gaseous zone 185. Liquidzone 275, gaseous zone 280, and boundary 290 may have characteristicssimilar to the characteristics of liquid zone 190, gaseous zone 185, andboundary 195, respectively, discussed above. For example, the size ofgaseous zones 280 and 185 may remain substantially constant, andboundaries 290 and 195 may remain relatively stationary, when the amountof heat imparted by higher speed (e.g., fast) neutrons and gammaradiation from fuel tubes 135 and the amount of heat removed by reactorcoolant subsystem 25 are substantially equal.

Passageway 210 may be formed between cone 215 and interior cone 235. Agap 300 may be formed between a bottom portion of cone 215 and a bottomportion of interior cone 235. Moderator may be free to move betweenpassageway 210 and a lower portion of control cavity 140 via gap 300,which may be similar to gap 230. Thus, because control cavity 140 may bein fluid communication with reflector zone 95, moderator may be free tomove between passageway 210 and reflector zone 95 via control cavity140. Because passageway 210 may not be closed at the top, passageway 210may be substantially filled with liquid moderator and moderator steambubbles may rise rapidly through it.

FIGS. 8A, 8B, 8C, and 8D illustrate alternative views of cone assembly150.

FIGS. 9, 10, and 11 illustrate a second exemplary embodiment of reactor15. In this embodiment, reactor 15 may include a reactor core 100′disposed in reflector zone 95. Reactor core 100′ may include a fuelassembly 125′ and a control cavity array 130′. Control cavity array 130′may confine moderator adjacent to fuel assembly 125′. In this secondembodiment, fuel tubes 135′ may be disposed horizontally and arranged ina square array with truncated corners, as illustrated in FIG. 10. Themoderator may be cold and may be cooled by pumping relatively coolermoderator into control cavities 140′. The moderator may be heavy water(D₂O), and the composition of the primary coolant may be any suitablecoolant.

Fuel assembly 125′ may include a plurality of fuel tubes 135′. Fueltubes 135′ may be similar to fuel tubes 135 of reactor core 100. Fueltubes 135′ may be, for example, substantially horizontally disposed.

Control cavity array 130′ may include a plurality of control cavities140′. As depicted in the end view of reactor core 100′ illustrated inFIG. 10, control cavities 140′ may be disposed between fuel tubes 135′of fuel assembly 125′. Each control cavity 140′ may be included in astructural assembly 145′ that may be a tube having a length greater thanthe length of fuel assembly 125′, and may contain control cavities 140′that may serve as housings to confine moderator.

As depicted in FIGS. 9 and 11, structural assembly 145′ may include oneor more upper members 155′, one or more end members 165′, and one ormore intermediate members 170′, which may be formed from similarmaterials and attached by similar techniques as the members ofstructural assembly 145 of control cavity 140. Upper member 155′ mayhave, for example, a curved shape that encloses an upper portion ofcontrol cavity 140′. For example, upper member 155′ may have asemi-circular shape that encloses an upper portion of control cavity140′. Also, for example, upper member 155′ may have a substantiallyfully circular shape with a lower portion 160′, so that upper member155′ that continues into lower portion 160′ may fully enclose controlcavity 140′. End members 165′ may be attached to end portions of uppermember 155′ and lower portions 160′ to fully enclose control cavities140′. Structural assembly 145′ may extend beyond the extent of fuel rods(that may be disposed in fuel tubes 135′) to include end compartments142′. End members 165′ may have a passageway 166′ that is in fluidcommunication with vertical standpipe 167′, which may allow liquidmoderator to flow out at a location near the top of end compartments142′, and may allow moderator steam to flow freely in either directionbetween end compartments 142′ and standpipe 167′. The lower end ofstandpipe 167′ may lead into moderator reservoir 168′, which may containboth liquid moderator and moderator steam. When upper member 155′ is,for example, a semi-circular shape, upper member 155′ and intermediatemembers 170′ may form a cavity having a closed upper portion and an openbottom portion. Thus, upper member 155′ and intermediate members 170′may substantially prevent moderator movement in and out of an upperportion of control cavity 140′, while allowing moderator to be free tomove in and out of a lower portion of control cavity 140′. When uppermember 155′ is, for example, a substantially full circle, intermediatemembers 170′ may only cover an upper portion of an open circularcross-section formed by upper member 155′ that includes lower portion160′. Thus, intermediate members 170′ and upper member 155′ having lowerportion 160′ may substantially prevent moderator movement in and out ofan upper portion of control cavity 140′, while allowing moderator tomove in and out of a lower portion of control cavity 140′.

One or more intermediate members 170′ may be disposed between andattached to an interior surface of upper member 155′. Intermediatemembers 170′ may be disposed at any interval along control cavity 140′.Intermediate members 170′ may substantially prevent movement ofmoderator through control cavity 140′ at an upper portion of controlcavity 140′. Intermediate members 170′ may have a height that is lessthan a height of control cavity 140′. Thus, intermediate members 170′may serve as baffles to block movement of moderator in an upper portionof control cavity 140′ and allow movement of moderator in a lowerportion of control cavity 140′. Moderator may be free to move through alower portion of control cavity 140′ by moving under intermediatemembers 170′, and may move between reflector zone 95, end compartments142′, and control cavity 140′ by moving under intermediate members 170′.

As depicted in FIGS. 9 and 11, control cavities 140′ may include thesame moderator as the moderator in end compartments 142′, becausemoderator may move between reflector zone 95 and control cavities 140′.As moderator confined in control cavity 140′ is heated by neutrons,gamma radiation, and thermal conduction from fuel tubes 135′, some orall of the moderator in control cavity 140′ may be heated into a gaseousstate in a gaseous zone 185′. Some or all of the moderator in controlcavity 140 may also be in a liquid state in a liquid zone 190′. Gaseouszone 185′ and liquid zone 190′ may be separated by a boundary 195′. Thesize of gaseous zone 185′ and liquid zone 190′ may vary between controlcavities 140′, and between different intermediate members 170′ within asingle structural assembly 145′. Thus, the location of boundary 195′ mayvary between control cavities 140′ and between different intermediatemembers 170′ within a single structural assembly 145′. For example, agiven control cavity 140′ may have both a gaseous zone 185′ and a liquidzone 190′, substantially only a gaseous zone 185′, or substantially onlya liquid zone 190′.

Liquid zone 190′, gaseous zone 185′, and boundary 195′ may havecharacteristics similar to the characteristics of liquid zone 190,gaseous zone 185, and boundary 195, respectively, discussed above withreference to control cavity 140. For example, the size of gaseous zone185′ may remain substantially constant, and boundary 195′ may remainrelatively stationary, when the amount of heat imparted by fastneutrons, gamma radiation, and conduction from fuel tubes 135′ and theamount of heat removed by reactor coolant subsystem 25 are substantiallyequal.

FIGS. 12A through 12F illustrate a third alternative exemplaryembodiment of reactor 15. This embodiment includes a hexagonal array ofvertical fuel tubes (for example, as illustrated in FIGS. 12A and 6) anda hot moderator that may be cooled by pumping hot moderator out of areflecting pool, cooling the hot moderator, and pumping the moderatorback into the reactor core and control cavities via reactor coolantsubsystem 25. In this embodiment (as illustrated in FIG. 12F), eachassembly of control cavities may fit vertically into the space boundedby four vertical fuel tubes. As illustrated in FIG. 12B, this embodimentmay include a reactor core 100 a.

Reactor core 100 a may include a fuel assembly 125 a that is similar tofuel assembly 125, and a control cavity array 130 a. Control cavityarray 130 a may contain a pocket of moderator and/or moderator steamadjacent to fuel assembly 125 a. In this embodiment, as described morefully below, a moderator coolant tube 335 a may have small holes 337 adisposed in the sides and extending along a length of moderator coolanttube 335 a, and control cavities 140 a may be cooled by a fine spray ofrelatively cooler moderator sprayed from the moderator coolant tube 335a.

Control cavity array 130 a may include a three-dimensional array ofcontrol cavities 140 a. For example, the three-dimensional array ofcontrol cavities 140 a may serve as a housing to compartmentalize and/orconfine pockets of moderator adjacent to fuel tubes 135 a of fuelassembly 125 a. As depicted in FIGS. 12A through 12F, the plurality ofcontrol cavities 140 a may be disposed in vertical stacks with thestacks disposed horizontally to each other as well as being stackedvertically. As depicted in FIG. 12E, control cavities 140 a may bestaggered vertically within control cavity array 130 a. Control cavities140 a may be arranged in any suitable configuration for confiningpockets of moderator and/or moderator steam adjacent to fuel tubes 135a.

As depicted in FIGS. 12C through 12F, each control cavity 140 a mayinclude moderator coolant tube 335 a, a roughly conical upper member 155a and a side member 160 a. As illustrated, side member 160 a may beroughly trapezoidal (for example, in the illustrated hexagonal fuel tubearray) with indented corners 161 a for fuel tubes 135 a or roughlysquare (not illustrated) for a square fuel tube array. Upper member 155a may be joined without gaps to side member 160 a and moderator coolanttube 335 a to confine a pocket of moderator and/or moderator steamadjacent to fuel tubes 135 a. Moderator may be free to move into or outof control cavity 140 a via the open bottom of control cavity 140 a andthrough a gap 162 a between the bottom of a given side member 160 a andthe top of side member 160 a of the cavity below.

Upper member 155 a, side member 160 a, and moderator coolant tube 335 amay be formed from any suitable structural materials for directingmoderator movement and/or confining moderator such as, for example,zirconium alloy. Upper member 155 a, side member 160 a, and moderatorcoolant tube 335 a may be attached to each other by any suitabletechnique such as, for example, welding. Upper member 155 a, side member160 a, and moderator coolant tube 335 a may also be integrally formedwith each other. Upper member 155 a, side member 160 a, and moderatorcoolant tube 335 a may be attached to form, for example, a cavity havinga closed upper portion and an open bottom portion. Thus, upper member155 a, side member 160 a, and moderator coolant tube 335 a maysubstantially prevent moderator movement in and out of an upper portionof control cavity 140 a, while allowing moderator to be free to move inand out of a lower portion of control cavity 140 a. The upper portion ofcontrol cavity 140 a may include upper member 155 a, upper portions ofside member 160 a, and portions of moderator coolant tube 335 a. Thelower portion of control cavity 140 a may include lower portions of sidemember 160 a, and portions of moderator coolant tube 335 a.

Gap 162 a may allow movement of moderator between reflector zone 95 andcontrol cavity 140 a, either directly or via a gap 182 a formed betweenadjacent, horizontally disposed control cavities 140 a or betweencontrol cavities 140 a and fuel tubes 135 a.

As depicted in FIGS. 12B and 12E, control cavities 140 a may include thesame moderator as reflector zone 95, because moderator may be free tomove between reflector zone 95 and control cavities 140 a via gaps 162 aand 182 a. As moderator confined in control cavity 140 a is heated byneutrons and gamma radiation emitted from fuel tubes 135 a, and heat isconducted from fuel tubes 135 a, some or all of the moderator in controlcavity 140 a may be heated into a gaseous state in a gaseous zone 185 a.Some or all of the moderator in control cavity 140 a may also be in aliquid state in a liquid zone 190 a. Gaseous zone 185 a and liquid zone190 a may be separated by a boundary 195 a. The size of gaseous zone 185a and liquid zone 190 a may vary between different control cavities 140a and within each control cavity 140 a at different times during anoperation of reactor 15.

Thus, the location of boundary 195 a may vary between control cavities140 a. For example, a given control cavity 140 a may have both a gaseouszone 185 a and a liquid zone 190 a, substantially only a gaseous zone185 a, or substantially only a liquid zone 190 a.

Heat imparted via neutrons, gamma radiation, and/or conduction from fueltubes 135 a may cause the liquid moderator of liquid zone 190 a to bemaintained at a temperature very near the boiling point of themoderator. For example, the moderator of liquid zone 190 a may bemaintained in a simmering state. As the moderator in liquid zone 190 asimmers, some moderator may evaporate and rise into gaseous zone 185 a.Moderator in liquid zone 190 a may be cooled by mixing with relativelycooler moderator passing into control cavity 140 a through small holes337 a in moderator coolant tube 335 a. Also, moderator in gaseous zone185 a may condense around droplets of a fine, relatively coolermoderator spray passing through small holes 337 a in moderator coolanttube 335 a, or may condense and drip back to liquid zone 190 a alonginner surfaces of control cavity 140 a and/or an outer surface ofmoderator coolant tube 335 a. The size of gaseous zone 185 a maytherefore remain substantially constant, and boundary 195 a may remainrelatively stationary, when the amount of heat imparted by neutrons andgamma radiation from fuel tubes 135 a and the amount of heat removed byreactor coolant subsystem 25 are substantially equal. As describedfurther below, the size of gaseous zone 185 a and a position of boundary195 a may vary slightly over short periods of time (e.g., over a periodof days) based on the xenon and samarium load of the fuel, and may varysignificantly over long periods of time (e.g., over a period of years),based on, for example, the age (or burnout) of the fuel. The size ofgaseous zone 185 a and the position of boundary 195 a may vary slightlyduring and shortly after periods of change in the rate of cooling byreactor coolant subsystem 25.

As illustrated in FIG. 12E, control cavities 140 a may be cooled bymovement of cooler moderator through moderator coolant tube 335 a andinto the control cavities 140 a through one or more holes 337 a locatedin the sides of moderator coolant tube 335 a. Holes 337 a may be anysuitable size for moderator movement such as, for example, holes thatare small in size. A substantially equal volume of warmer moderator maythen move out of the control cavity 140 a into the reflector zone 95 viagap 162 a at the lower portion of control cavity 140 a.

As depicted in FIGS. 12C and 12D, the lower part of reflector zone 95may be cooled by movement of cooler moderator from moderator coolanttube 335 a through one or more small holes 338 a located in a cap on alower end of moderator coolant tube 335 a.

FIG. 12G provides a perspective view of the arrangement of controlcavities 140 a of reactor core 100 a. It is contemplated that thevarious disclosed elements of reactors 100, 100′, 100 a and/or 100 b maybe used in combination with each other.

FIGS. 12H through 12M depict a fourth embodiment with an array ofvertical fuel tubes and hot moderator cooled by pumping hot moderatorout of reflecting pool 105 and control cavity array 130 b, cooling it,and pumping the cooler moderator back into control cavity array 130 band reflecting pool 105. In this embodiment, each assembly of controlcavities may be an annular stack of control cavities surrounding asingle vertical fuel tube. As illustrated in FIG. 12H, this embodimentmay include a reactor core 100 b.

Reactor core 100 b may include a fuel assembly 125 b, which is similarto fuel assembly 125, and a control cavity array 130 b. Control cavities140 b of control cavity array 130 b may contain a pocket of moderatorand/or moderator steam adjacent to fuel assembly 125 b.

Fuel assembly 125 b may be any type of nuclear fuel suitable for use ina nuclear reaction. For example, as illustrated in FIG. 12J, fuelassembly 125 b may include bundles of fuel rods 127 b that are disposedin a plurality of fuel tubes 135 b. For example, fuel assembly 125 b mayinclude an arrangement of dozens to hundreds of fuel tubes 135 b. Forexample, fuel assembly 125 b may include between about 19 and about 500fuel tubes 135 b that are about three inches to about 18 inches indiameter. Each fuel tube 135 b may include a single fuel bundle ofrelatively long fuel rods 127 b or any suitable number of fuel bundlessuch as, for example, 12 fuel bundles of relatively short fuel rods 127b. Each fuel bundle may include any suitable number of fuel rods 127 bbetween about 19 and about 1231 fuel rods such as, for example, 37 fuelrods. Fuel assembly 125 b may include any suitable fuel for a nuclearreaction such as, for example, natural uranium, enriched uranium,plutonium, or thorium, individually or in various mixtures. Fuel rods127 b may be cast metallic fuel, or rods of fuel or fuel oxide pelletsin a cladding tube (e.g., a zirconium alloy tube). For example, fuelassembly 125 b may include a mixed uranium/plutonium fuel or a mixedfuel of used light water reactor fuel and thorium. Fuel tubes 135 b mayalso contain fuel in forms other than rods such as, for example, spheresor pebbles. Fuel tubes 135 b may also contain a molten salt in which themetallic ion of the salt is an ion of the fuel, and the molten saltfunctions both as the fuel and the coolant.

Each fuel tube 135 b may contain primary coolant in addition to thefuel. The primary coolant may include any material in a suitable fluidstate such as, for example, heavy water, light water, suitable liquidmetal (e.g., lead or sodium), suitable molten salts, suitable organicfluids, and/or a suitable gas (e.g., helium).

Fuel assembly 125 b may include fuel tubes 135 b that are verticallydisposed (e.g., as illustrated in FIG. 2). Fuel assembly 125 b mayinclude fuel tubes 135 b arranged in any suitable configuration such as,for example, a right angle array as illustrated in FIGS. 4 and 5. Fuelassembly 125 b may also include, for example, fuel tubes 135 b that arearranged in a hexagonal array as illustrated in FIG. 6. Fuel tubes 135 bmay be, for example, disposed substantially vertically.

Referring back to FIGS. 12H through 12M, control cavity array 130 b mayinclude a three-dimensional array of control cavities 140 b. Forexample, the three-dimensional array of control cavities 140 b may serveas a housing to compartmentalize and/or confine pockets of moderatoradjacent to fuel tubes 135 b of fuel assembly 125 b. As depicted inFIGS. 12H through 12M, the plurality of control cavities 140 b may bedisposed in vertical stacks with the stacks disposed horizontally toeach other as well as being stacked vertically. Control cavities 140 bmay be staggered vertically within control cavity array 130 b. Controlcavities 140 b may be arranged in any suitable configuration forconfining pockets of moderator and/or moderator steam adjacent to fueltubes 135 b.

As depicted in FIGS. 12J through 12M, each control cavity 140 b mayinclude a moderator coolant inflow tube 335 b, a moderator outflow tube337 b, a slanted upper member 155 b, and side members 160 b and 162 b.As depicted in FIG. 12L, side member 160 b may be, for example, roughlycircular or roughly hexagonal for a hexagonal fuel tube array, orroughly square for a square fuel tube array. Upper member 155 b may bejoined without gaps to side members 160 b and 162 b, moderator coolantinflow tube 335 b, and/or moderator outflow tube 337 b to confine apocket of moderator and/or moderator steam adjacent to fuel tubes 135 b.Moderator may be free to move between control cavity 140 b and moderatorcoolant outflow tube 337 b via a hole 338 b located at the lower portionof each control cavity 140 b.

Upper member 155 b, side members 160 b and 162 b, and tubes 335 b and337 b may be formed from any suitable structural materials for directingmoderator movement or confining moderator such as, for example,zirconium alloy. Upper member 155 b, side members 160 b and 162 b, andtubes 335 b and 337 b may be attached to each other by any suitabletechnique such as, for example, welding. Upper member 155 b, sidemembers 160 b and 162 b, and tubes 335 b and 337 b may also beintegrally formed with each other. Upper member 155 b, side members 160b and 162 b, and tubes 335 b and 337 b may be attached to form, forexample, a cavity having a closed upper portion and an open bottomportion. Thus, upper member 155 b, side members 160 b and 162 b, andtubes 335 b and 337 b may substantially prevent moderator movement inand out of an upper portion of control cavity 140 b, while allowingmoderator to move in and out of a lower portion of control cavity 140 b.The upper portion of control cavity 140 b may include upper member 155b, upper portions of side members 160 b and 162 b, and portions of tubes335 b and 337 b. The lower portion of control cavity 140 b may includelower portions of side members 160 b and 162 b, and portions of tubes335 b and 337 b. Hole 338 b and moderator outflow tube 337 b may allowmovement of moderator between reflector zone 95 and control cavities 140b. Moderator coolant inflow tube 335 b may be sealed at its top end (forexample, in an uppermost control cavity 140 b associated with a givenfuel tube 135 b, as illustrated in FIG. 12K). A gap 180 b may bedisposed between control cavities 140 b and fuel tubes 135 b, and may befilled with an inert gas or other suitable material, and may be closedat a top and/or a bottom portion to contain such material or to reduceconvection circulation.

As depicted in FIGS. 12I and 12L, control cavities 140 b may includesubstantially the same moderator as reflector zone 95, because moderatormay move between reflector zone 95 and control cavities 140 b viamoderator outflow tube 337 b and hole 338 b. As moderator confined incontrol cavity 140 b is heated by neutrons and gamma radiation emittedfrom fuel tubes 135 b and by thermal conduction from fuel tube 135 b,some or all of the moderator in control cavity 140 b may be heated intoa gaseous state in a gaseous zone 185 b. Some or all of the moderator incontrol cavity 140 b may also be in a liquid state in a liquid zone 190b. Gaseous zone 185 b and liquid zone 190 b may be separated by aboundary 195 b. The size of gaseous zone 185 b and liquid zone 190 b mayvary between different control cavities 140 b. Thus, the location ofboundary 195 b may vary between control cavities 140 b. For example, agiven control cavity 140 b may have both a gaseous zone 185 b and aliquid zone 190 b, substantially only a gaseous zone 185 b, orsubstantially only a liquid zone 190 b.

Heat imparted via neutrons, gamma radiation, and/or thermal conductionfrom fuel tubes 135 b may cause the liquid moderator of liquid zone 190b to be maintained at a temperature very near the boiling point of themoderator. For example, the moderator of liquid zone 190 b may bemaintained in a simmering state. As the moderator in liquid zone 190 bsimmers, some moderator may evaporate and rise into gaseous zone 185 b.Also, moderator in gaseous zone 185 b that is near moderator coolantinflow tube 335 b or that has cool moderator sprayed into it frommoderator coolant inflow tube 335 b via holes 336 b may condense anddrip back to liquid zone 190 b of control cavity 140 b. Holes 336 b maybe any suitable size for moderator movement such as, for example, holesthat are small in size. The size of gaseous zone 185 b may thereforeremain substantially constant, and boundary 195 b may remain relativelystationary, when the amount of heat imparted into each control cavity140 b by fuel tubes 135 b (e.g., by heat transfer, neutron slowing,and/or gamma radiation) and the amount of heat removed by the inflow ofcooler moderator are substantially equal. As described further below,the size of gaseous zone 185 b and a position of boundary 195 b may varyslightly over short periods of time (e.g., over a period of hours ordays) based on the xenon and samarium load of the fuel, and may varysignificantly over long periods of time (e.g., over a period of years),based on, for example, the age (or burnout) of the fuel. The size ofgaseous zone 185 b and the position of boundary 195 b may vary slightlyduring and shortly after periods of change in the rate of cooling byreactor coolant subsystem 25.

As illustrated in FIG. 12J, control cavities 140 b may be cooled bymovement of cooler moderator through moderator coolant inflow tube 335 band into control cavities 140 b through holes 336 b in the sides ofmoderator coolant inflow tube 335 b. A substantially equal volume ofwarmer moderator may move out of control cavity 140 b into reflectorzone 95 and to reactor coolant subsystem 25 via hole 338 b and moderatoroutflow tube 337.

As depicted in FIGS. 12I, 12J, and 12K, the lower portion of reflectorzone 95 may be cooled by flow of cooler moderator from moderator coolantinflow tube 335 b through holes 336 b in the lower portion of moderatorcoolant inflow tube 335 b, with excess moderator flowing to moderatorcoolant subsystem 315 (described below) via moderator coolant outflowtube 337 b.

As depicted in FIGS. 12I, 12J, and 12K, the upper portion of reflectorzone 95 and control cavity array 130 b may be cooled by evaporationoccurring at boundary 115. During the evaporation, excess steammoderator may move into moderator coolant subsystem 315 (describedbelow) via a transfer tube 323 b.

As depicted in FIG. 12N, a tank 377 b containing unpressurized water(H₂O) may include a plurality of moderator heat exchange tubes 390 bthat are fluidly connected to a moderator coolant tube 327 b. Moderatorheat exchange tubes 390 b may extend through the unpressurized water(H₂O) contained in tank 377 b, and may be fluidly connected via apassageway 355 b with a moderator coolant pump 350 b. A passageway 322 bmay fluidly connect moderator coolant pump 350 b to moderator coolantinflow tube 335 b that is disposed in control cavity array 130 b. Asteam pressure control valve 380 b may allow the passage of some steammoderator from steam transfer tube 323 b to a plurality of steam heatexchange tubes 385 b when a pressure in steam transfer tube 323 b isgreater than a desired pressure. Moderator steam in steam heat exchangetubes 385 b may condense on inside walls of steam heat exchange tubes385 b or may escape out of a bottom portion of steam heat exchange tubes385 b and condense in the cool moderator disposed in moderator heatexchange tube 390 b.

Tank 377 b may be any suitable tank for being substantially filled withunpressurized water (H₂O) so that the temperature may not exceed theboiling point of water (H₂O). In normal operation, tank 377 b may becooled by any suitable method to just below the boiling point of water(H₂O). In a situation where power to reactor 15 is disrupted, or anothersituation where normal cooling operates abnormally, tank 377 b may becooled by evaporation from the surface of the water (H₂O) disposed intank 377 b.

As illustrated in FIG. 13, reactor coolant subsystem 25 may include atransfer subsystem 305, a fuel coolant subsystem 310, and a moderatorcoolant subsystem 315. Transfer subsystem 305 may transfer reactorcoolant between heat exchanger 20 and reactor core 100, 100′, 100 a,and/or 100 b. Fuel coolant subsystem 310 may facilitate heat exchangefrom fuel tubes 135, 135′, 135 a, and 135 b, and moderator coolantsubsystem 315 may facilitate heat exchange from control cavities 140′,140 a, 140 b, and reflector zone 95.

The reactor coolant of reactor coolant subsystem 25 may be any suitablefluid material for facilitating heat exchange from reactor core 100,100′, 100 a, and/or 100 b. For example, the reactor coolant may includeD₂O (“heavy water”), H₂O (“light water”), molten metal or salt, or agas. A similar coolant may be used for fuel coolant subsystem 310 andmoderator coolant subsystem 315, or a different coolant may be used forfuel coolant subsystem 310 and moderator coolant subsystem 315.

Transfer subsystem 305 may include a cold reactor coolant passageway 320and a hot reactor coolant passageway 325. Passageways 320 and 325 may beformed from any suitable material for transferring reactor coolant suchas, for example, steel and/or zirconium alloy. The same passageway 320and passageway 325 may transfer reactor coolant for both fuel coolantsubsystem 310 and moderator coolant subsystem 315 (as in, e.g., thefirst exemplary embodiment), or separate passageways 320 and 325 may beprovided for fuel coolant subsystem 310 and passageways 322 a, 327 a,322 b, 327 b, and similar passageways in reactor core 100′ (not shown)for moderator coolant subsystem 315. Cold reactor coolant passageway 320may transfer cold reactor coolant from heat exchanger 20 to reactor 15.The cold reactor coolant may be in a liquid state and may be anysuitable temperature for facilitating heat exchange from reactor 15.

Referring back to FIG. 2, for example, cold reactor coolant passageway320 may pass through apertures of containment structure 85 and intoreflector zone 95. Cold reactor coolant passageway 320 may communicatewith passageways of fuel coolant subsystem 310 and moderator coolantsubsystem 315 inside of reflector zone 95, and may thereby supply fuelcoolant subsystem 310 and moderator coolant subsystem 315 with coldreactor coolant for heat exchange. Hot reactor coolant passageway 325may be in fluid communication with fuel coolant subsystem 310 andmoderator coolant subsystem 315, and may receive hot reactor coolant(e.g., reactor coolant that has passed through reactor core 100, 100′,100 a, and/or 100 b in fuel tubes 135, 135′, 135 a, and/or 135 b,thereby facilitating heat exchange with reactor core 100, 100′, 100 a,and/or 100 b) from fuel coolant subsystem 310 and moderator coolantsubsystem 315. Hot reactor coolant passageway 325 may transfer hotreactor coolant from reactor 15 back to heat exchanger 20.

As illustrated, for example, in FIG. 3, fuel coolant subsystem 310 mayinclude a plurality of passageways 330 that may be in fluidcommunication with cold reactor passageway 320 and hot reactor coolantpassageway 325 of transfer subsystem 305. Cold reactor coolant may flowfrom cold reactor passageway 320 to passageways 330. Passageways 330 maybe disposed leading to and from fuel tubes 135, 135′, 135 a, and/or 135b. Cold reactor coolant may pass through passageways 330, therebypassing through fuel tubes 135, 135′, 135 a, and/or 135 b to facilitateheat exchange with fuel tubes 135, 135′, 135 a, and/or 135 b. The coldreactor coolant may be heated by fuel disposed in tubes 135, 135′, 135a, and/or 135 b, and may be transferred out of fuel tubes 135, 135′, 135a, and 135 b via passageways 330. Passageways 330 may then transfer thehot reactor coolant to hot reactor coolant passageway 325 of transfersubsystem 305. The hot reactor coolant may be in a substantially fullyliquid state, may be in a partially liquid state and a partially gaseousstate, or may be in a substantially fully gaseous state.

As illustrated, for example, in FIG. 2, moderator coolant subsystem 315may include a plurality of passageways 335 that may be in fluidcommunication with cold reactor coolant passageway 320 and hot reactorcoolant passageway 325 of transfer subsystem 305. Cold reactor coolantmay flow from cold reactor coolant passageway 320 to passageways 335 and330. The cold reactor coolant may be in a liquid state. Passageways 335may be disposed within control cavities 140. Cold reactor coolant maypass through passageways 335, thereby passing through control cavities140 to facilitate heat exchange with control cavities 140. The coldreactor coolant may be heated by moderator confined within controlcavities 140 into warm reactor coolant, and may be transferred out ofcontrol cavities 140 via passageways 335. Similar to the heat exchangeperformed by passageways 335 in the disclosed control cavities,passageways 330 may transfer cold reactor coolant from cold reactorcoolant passageway 320 through reflecting pool 105. It is alsocontemplated that the cold reactor coolant may be heated by themoderator of reflecting pool 105 into warm reactor coolant. Passageways335 and 330 may then transfer the warm reactor coolant to a lowerportion of fuel tubes 135, through the fuel tubes 135 (where it isheated by the fuel to become hot reactor coolant), and then to hotreactor coolant passageway 325 of transfer subsystem 305. The hotreactor coolant may be in a substantially fully liquid state or may bein a partially liquid state and a partially gaseous state.

FIG. 14 illustrates an exemplary detailed illustration of passageway 335as it passes through control cavities 140 for facilitating heat exchangefrom control cavities 140. Passageway 335 may be connected to coldreactor coolant passageway 320 and/or hot reactor coolant passageway 325of transfer subsystem 305 either directly or via an intermediatepassageway 345. Passageway 335 may include an entry member 350, aninterior member 355, an exterior member 360, and an exit member 365.Entry member 350 may fluidly connect intermediate passageway 345 withinterior member 355. Interior member 355 may be disposed within aninterior of exterior member 360. For example, interior member 355 andexterior member 360 may be an arrangement of concentric tubes. Exitmember 365 may fluidly connect exterior member 360 with intermediatepassageway 345. Entry member 350 may pass through an aperture in a wallof exit member 365, and may be partially disposed within exit member365. Interior member 355 may have an end portion 370 that may be open. Aplurality of apertures 375 may be formed through a wall of interiormember 355. Apertures 375 may increase in size, and a spacing betweenapertures 375 may decrease, in a direction moving toward end portion 370of interior member 355. Reactor coolant may flow from entry member 350and through a channel 380 of interior member 355. Some reactor coolantmay pass through apertures 375 and into a channel 385, before reachingopen end portion 370 of interior member 355. A size and frequency ofapertures 375 may increase, in a direction moving toward end portion370, and an amount of mixing of reactor coolant between channels 380 and385 may increase in a direction moving toward end portion 370. Channel385 may be formed between interior member 355 and exterior member 360,and may be an annular-shaped channel. After passing through apertures375 and/or open end portion 370, reactor coolant may flow throughchannel 385 and into intermediate passageway 345, via exit member 365.Reactor coolant disposed in channel 385 may be heated by thermalconduction from the warmer moderator in control cavity 140 through thewall of exterior member 360. By allowing some flow of relatively coolercoolant from channel 380 to channel 385 via apertures 375, thetemperature of coolant in channel 385 may be relatively constant alongits length. Heat transfer fins (not shown) may be added to the innerand/or outer surfaces of exterior member 360 to facilitate the heattransfer.

Referring back to FIG. 13, pump subsystem 30 may include a coolant pump390, an H₂O pump 395, and a motor 400. Motor 400 may drive coolant pump390 and H₂O pump 395.

Coolant pump 390 may be any suitable type of pump for pressurizing flowof reactor coolant in transfer subsystem 305. For example, coolant pump390 may be a positive displacement pump such as a rotary-type pump, areciprocating-type pump, or a linear-type pump. Also, for example,coolant pump 390 may be a steam pump, an impulse pump, a hydraulic rampump, or a centrifugal pump. Coolant pump 390 may pressurize a flow ofreactor coolant in cold reactor coolant passageway 320 from heatexchanger 20 to reactor 15, and within hot reactor coolant passageway325 from reactor 15 back to heat exchanger 20. Coolant pump 390 maypressurize the same reactor coolant in transfer subsystem 305 for bothfuel coolant subsystem 310 and moderator coolant subsystem 315, or oneor more coolant pumps 390 may separately pressurize reactor coolant forfuel coolant subsystem 310 and cool moderator for moderator coolantsubsystem 315.

H₂O pump 395 may be of a type similar to coolant pump 390 and maypressurize a flow of water (H₂O) and steam (H₂O) in turbine steamsubsystem 65. H₂O pump 395 may pressurize a flow of hot steam (H₂O) inpassageway 70 from heat exchanger 20 to turbine 45, a flow of surplus ordead steam (H₂O) in passageway 75 from turbine 45 to turbine coolingsubsystem 60, and a flow of water (H₂O) in passageway 80 from turbinecooling subsystem 60 to heat exchanger 20.

Motor 400 may be any suitable type of motor for driving coolant pump 390and H₂O pump 395 such as, for example, a fixed or variable-displacementmotor, a bent-axis type hydraulic motor, a linear hydraulic motor, ahydraulic cylinder or an electric motor. Motor 400 may drive coolantpump 390 and H₂O pump 395 in any suitable manner such as, for example,via one or more mechanical shafts 405. For example, motor 400 may driveboth coolant pump 390 and H₂O pump 395 via a single mechanical shaft405. Mechanical shaft 405 may include a flywheel that operates tomitigate rapid flow changes as motor 400 drives coolant pump 390 and H₂Opump 395. Motor 400 may also drive coolant pump 390 and H₂O pump 395separately. It is also contemplated that motor 400 may drive pump 390and H₂O pump 395 by other suitable techniques such as, for example,hydraulically. Motor 400 may be configured to drive both coolant pump390 and H₂O pump 395 at an optimized level when nuclear reactor system 5is operating at full power. Motor 400 may drive both coolant pump 390and H₂O pump 395 when motor 400 is shut down or stops operating, andboth coolant pump 390 and H₂O pump 395 may also simultaneously shutdown. It is also contemplated that each pump may have a separate motor.

As illustrated in FIGS. 16-18, auxiliary coolant subsystem 35 mayinclude a convection loop subsystem 410 and an auxiliary heat exchangesubsystem 415. Convection loop subsystem 410 and auxiliary heat exchangesubsystem 415 may provide auxiliary systems for facilitating heatexchange from reactor 15.

As illustrated in FIG. 16, convection loop subsystem 410 may include ajunction 425, a passageway 430, a passageway 435, a plurality ofpassageways 440 and 445, a merging portion 450, a junction 455, a valve460, and valve 465. Junction 425, passageway 430, passageway 435, theplurality of passageways 440 and 445, merging portion 450, and junction455 may be formed from any material suitable for transferring reactorcoolant, and may be in fluid communication to provide an auxiliaryreactor coolant path. Junction 425 may be configured to maintain apressure A at an inlet of passageway 430. A portion of reactor coolantflowing through hot reactor coolant passageway 325 may flow intopassageway 430 at junction 425. Passageway 430 may guide reactor coolantflow downward, below boundary 115 of reflector zone 95, thereby guidingflow below a top surface of reflecting pool 105. Reactor coolant mayflow from passageway 430, upward through passageway 435, and then towardcontainment structure 85 and pressure vessel 90 via the plurality ofpassageways 440. The plurality of passageways 440 may be in fluidcommunication with the plurality of passageways 445. The plurality ofpassageways 440 and 445 may be sized to be smaller than passageways 430and 435, and may be, for example, a plurality of small tubes. Theplurality of passageways 445 may be disposed adjacent to a surface ofpressure vessel 90 so as to have good heat exchange with pressure vessel90. For example, the plurality of passageways 445 may be welded topressure vessel 90. The plurality of passageways 445 may transferreactor coolant downward along pressure vessel 90, to a position near orbelow a bottom of reactor core 100, 100′, 100 a, and/or 100 b.

The plurality of passageways 445 may be fluidly connected with and mergeinto one or more merging portions 450, which may be larger than theplurality of passageways 445. For example, several passageways 445 maymerge into each of a plurality of larger merging portions 450. One ormore merging portions 450 may fluidly connect to cold reactor coolantpassageway 320 at junction 455. Junction 455 may be configured tomaintain a pressure B at an outlet of one or more merging portions 450such that when coolant pump 390 is providing a flow of coolant for fullpower operation, the pressure A at passageway 430 may balance thepressure B so that relatively little coolant passes between junction 425and junction 455 via passageways 430, 435, 440, 445, and merging portion450. When pump 390 is not operating and reactor core 100 is stillproducing heat, the hot coolant in fuel tubes 135 may rise and flow intopassageway 430 because passageway 325 may be substantially blocked bypump 390. The hot coolant may continue through passageways 435 and 440to the plurality of passageways 445. In passageways 445, the coolant maytransfer heat to reflector zone 95 and pressure vessel 90, and maybecome denser as it cools. This relatively denser moderator may fallthrough passageway 445 and junction 455 and displace relatively hottermoderator in fuel tubes 135, thus creating a convection circuit whichmay cool fuel tubes 135.

Valves 460 and 465 may be provided to isolate a flow of reactor coolantwithin convection loop subsystem 410 in the case of an interruption offlow and/or loss of coolant, external to reactor 15, of reactor coolantsubsystem 25. Valve 460 may be disposed in cold reactor coolantpassageway 320, and may be any suitable valve for substantially blockingflow of reactor coolant out of reactor 15. For example, valve 460 may bea one-way valve or a reverse blocking valve that may allow reactorcoolant to flow into reactor 15 via cold reactor coolant passageway 320,but may substantially block a flow of reactor coolant out of reactor 15via cold reactor coolant passageway 320. For example, valve 460 may bedisposed in cold reactor coolant passageway 320 at a position at or nearan exterior surface of containment structure 85. Valve 465 may bedisposed in hot reactor coolant passageway 325, and may be any suitablevalve for substantially blocking flow of reactor coolant out of reactor15 when the amount of reactor coolant is less than a threshold amount.For example, valve 465 may be a floating valve that may allow reactorcoolant to flow out of reactor 15 via hot reactor coolant passageway 325when the level of reactor coolant is greater than the threshold amount,but may substantially block a flow of reactor coolant out of reactor 15via hot reactor coolant passageway 325 when the level of reactor coolantis less than the threshold amount. For example, valve 465 maysubstantially block the flow of reactor coolant out of reactor 15 whenhot reactor coolant passageway 325 is less than half-full of reactorcoolant. Valve 465 may be disposed in hot reactor coolant passageway 325at a position at or near an exterior surface of containment structure85.

As illustrated in FIGS. 17 and 18, auxiliary heat exchange subsystem 415may include one or more heat exchange members 470, one or more heatexchange members 475, and one or more heat exchange members 480. Heatexchange member 470, heat exchange member 475, and heat exchange member480 may facilitate heat exchange for heat produced by reactor core 100,100′, 100 a, or 100 b to a location away from reactor 15.

Heat exchange member 470 may be an elongated element for housing amaterial. Heat exchange member may be disposed in containment structure85 (e.g., cast inside of a wall of containment structure 85), and may bedisposed near pressure vessel 90 or in contact with an exterior surfaceof pressure vessel 90. Heat exchange member 470 may be disposed radiallyin containment structure 85, so that one end of heat exchange member 470may be adjacent to or in contact with pressure vessel 90, and anotherend of heat exchange member 470 may be near an exterior portion ofcontainment structure 85. For example, heat exchange member 470 may bean elongated cavity that houses a state-changing material. For example,heat exchange member 470 may include a cavity that houses a metal alloy.For example, heat exchange member 470 may be a steel tube that is filledwith a metal alloy. The state-changing metal alloy may be a materialthat has a melting point that is slightly higher than a normal operatingtemperature of the moderator of reflector zone 95. For example, heatexchange member 470 may be a hollow steel tube that is substantiallyentirely filled with lead, tin, and/or any other material with asuitable melting point. If the temperature of the moderator withinreflector zone 95 exceeds its normal operating temperature, thestate-changing material housed within heat exchange member 470 may beheated from a solid state into a liquid state. For example, heatexchange member 470 may include lead as a state-changing material, whichmay be melted into molten lead when the moderator within reflector zone95 exceeds its normal operating temperature. When the state-changingmaterial changes states (e.g., when the lead melts), the conductivityproperties of the state-changing material may improve. Therefore, thestate-changing material of heat exchange member 470 may efficientlytransfer heat (for example, by convection) away from pressure vessel 90,and toward an exterior of containment structure 85 (which may have lowthermal conductivity), as the state-changing material melts. It is alsocontemplated that the state-changing material housed within heatexchange member 470 may be in a liquid state at normal moderatoroperating temperatures, and may be heated into a gaseous state when thetemperature of the moderator exceeds a normal operating temperature.

Heat exchange member 475 may also be an elongated cavity that houses astate-changing material, similar to heat exchange member 470. Thestate-changing material of heat exchange member 475 may be a materialwith a lower melting and/or boiling point than the state-changingmaterial of heat exchange member 470. For example, the state-changingmaterial may be a material in a liquid state, and may have a boilingpoint that is less than the temperature at which heat exchange member470 undergoes a state change (e.g., the melting point of lead or anyother suitable state-changing material of heat exchange member 470). Forexample, heat exchange member 475 may be a steel tube that is filledwith water (H₂O) or any other suitable material in a liquid state. Heatexchange member 475 may be disposed substantially vertically withincontainment structure 85 (e.g., cast within a wall of containmentstructure 85). As illustrated in FIGS. 17 and 18, heat exchange member475 may be in contact with or disposed near an end portion of one ormore heat exchange members 470, and may be disposed near an exteriorsurface of containment structure 85. The state-changing material of heatexchange member 475 may be heated by heat transferred from heat exchangemember 470, and may undergo a state change. For example, heattransferred from an end portion of heat exchange member 470 to heatexchange member 475 may cause the state-changing material to changestates (e.g., may cause water housed in the steel tube to boil). It isalso contemplated that the state-changing material of heat exchangemember 475 may be in a solid state at normal moderator operatingtemperatures, and may be heated into a liquid state when the temperatureof the moderator exceeds a normal operating temperature.

Heat exchange member 480 may be similar to heat exchange member 475, andmay be in fluid communication with heat exchange member 475. Thestate-changing material of heat exchange member 475 may thus flow fromheat exchange member 475 into heat exchange member 480. Heat exchangemember 480 may be disposed at a slight angle from a substantiallyhorizontal plane. Heat exchange member 480 may be disposed at a slightgrade such as, for example, 1 in 20 (rise over run) or 1 in 50 (riseover run). As illustrated in FIG. 18, heat exchange members 480 may fanout from reactor 15, thereby transferring heat away from reactor 15.Heat exchange members 480 may be disposed under a ground surface,thereby transferring heat from reactor 15 under any suitable amount ofground surface. For example, heat exchange members 480 may be disposedunder a large field and/or parking lot, thereby utilizing the largethermal capacity of the ground to absorb heat, and utilizing the groundsurface to dissipate heat. Because heat exchange member 480 may be at aslight slope, the state-changing material housed within heat exchangemember 480 may be cooled at a given distance from reactor 15 into theprevious state. For example, heat exchange member 475 may include waterthat may be heated into steam (H₂O) and transferred into heat exchangemember 480. At an outer end, heat exchange member 480 may terminate in asmall tank or reservoir of water so that heat exchange members 475 and480 are substantially always full of water. Heat exchange member 480 maybe a corrugated pipe configured to increase a contact area of the pipe(e.g., increase the contact area per unit of distance along the ground),and also increasing the contact area of any steam (H₂O) in the pipe withthe pipe interior surface. Because the steam (H₂O) traveling outwardalong the upper surface of the water (H₂O) in the pipe fills the upperportion of each corrugation in the pipe before any steam (H₂O) cantravel further out in the pipe, the corrugation increases the surfacearea of water (H₂O) in the pipe that is in contact with the steam (H₂O).After a given distance, enough heat may be dissipated such that thesteam (H₂O) condenses into water (H₂O).

As illustrated in FIG. 19, an auxiliary reactor shutdown subsystem 420may include a pressurized reservoir 485, one or more passageways 490, adrain passageway 495, and a pump 500. Pressurized reservoir 485 maysupply pressurized water (H₂O) into passageway 490. Pump 500 maypressurize water (H₂O) in drain passageway 495.

Pressurized reservoir 485 may be any suitable container for storingpressurized liquid such as, for example, a pressurized steel vessel. Anysuitable neutron-absorbing material may be stored in pressurizedreservoir 485 such as, for example, water (H₂O). Also, borated water(H₂O), having boron absorbed mixed into the water (H₂O), may be storedin pressurized reservoir 485. Pressurized reservoir 485 may be disposedon an exterior side of containment structure 85, and may include a valve487 that may be opened and closed to flow to selectively allow and blockflow of pressurized material from pressurized reservoir 485 into one ormore passageways 490.

Passageway 490 may be any suitable passageway for transferring apressurized material. Passageway 490 may be fluidly connected topressurized reservoir 485, and may transfer pressurized material frompressurized reservoir 485, through an aperture of containment structure85, and may split into one or more U-shaped tubes that pass down throughthe core area into reflector zone 95 below reactor core 100, 100′, 100a, or 100 b, and then back up through reactor core 100, 100′, 100 a, or100 b. Passageway 490 may transfer pressurized material throughreflector zone 95 and reactor core 100, 100′, 100 a, or 100 b in anysuitable manner. For example, as illustrated in FIG. 19, passageway 490may enter an upper portion of reflecting pool 105 and form asubstantially U-shaped configuration. Passageway 490 may be formed inany suitable configuration within reflector zone 95. When valve 487 isblocking flow of pressurized material from pressurized reservoir 485into passageway 490, passageway 490 may already be filled with steam(H₂O). When a fast shutdown of the reactor is desired (e.g., SCRAM),valve 487 is opened and pressurized neutron-absorbing material such as,for example, borated water (H₂O) fills passageway 490, the pressurizedneutron-absorbing material may increasingly pressurize the steam (H₂O)that was previously disposed in passageway 490. Therefore, the steam(H₂O) previously disposed in passageway 490 may be increasinglypressurized at an end portion 505 of each of the one or more passageways490, slowing and gradually stopping further flow.

Drain passageway 495 may disposed at a lower portion of reflecting pool105 and may fluidly connect any portion (e.g., a lower portion) ofpassageway 490 with pressurized reservoir 485. Pump 500 may be disposedin drain passageway 495 and may pressurize the neutron-absorbingmaterial to flow from the lower portion of passageway 490 back topressurized reservoir 485 when it is desired to restart reactor 15. Pump500 may also pressurize neutron-absorbing material disposed inpressurized reservoir 485. Pump 500 may thereby pump theneutron-absorbing material such as, for example, borated water (H₂O),from passageway 490 back to pressurized reservoir 485.

As illustrated in FIG. 20, reactor control subsystem 40 may include acontrol subsystem 510, a load-following subsystem 515, a bypasssubsystem 520, a moderator stabilization subsystem 525, a reactorcoolant stabilization subsystem 530, and a differential flow subsystem535. Control subsystem 510, load-following subsystem 515, bypasssubsystem 520, moderator stabilization subsystem 525, reactor coolantstabilization subsystem 530, and differential flow subsystem 535 maycontrol and/or stabilize an operation of nuclear reactor system 5.

Control subsystem 510 may include a controller 540 that may be any typeof programmable logic controller suitable for automating machineprocesses. Controller 540 may be connected to the components of nuclearreactor system 5 via electrical lines (not shown), and may control anoperation of any suitable component of nuclear reactor system 5 via theelectrical lines. For example, controller 540 may be electricallyconnected to and control components of power generation subsystem 10,reactor 15, heat exchanger 20, reactor coolant subsystem 25, pumpsubsystem 30, auxiliary coolant subsystem 35, and/or reactor controlsubsystem 40. Control subsystem 510 may also include input and/or outputcomponents that are in electrical communication with controller 540 suchas, for example, displays, monitors, keyboards, and other devices foruse by operators of nuclear reactor system 5. Control subsystem 510 mayalso include sensors that are disposed in the various passageways andcomponents of nuclear reactor system 5. The sensors may measure anysuitable parameter such as, for example, a temperature and/or pressureof, e.g., H₂O or reactor coolant. The sensors may be electricallyconnected to controller 540, and may input sensed data to controller 540for use in the control of nuclear reactor system 5.

Load-following subsystem 515 may include gates 545 and 550, passageways555, 560, 565, 580, and 590, a condenser 570, a valve 575, a heatexchanger 585, and a junction 595, which may be any suitable elementsfor transferring steam (H₂O) and water (H₂O).

Gate 545 may be disposed in passageway 70 and may selectively allow flowfrom passageway 70 into passageway 555. Gate 545 may be selectivelymoved from a closed position that substantially blocks flow of steam(H₂O) from passageway 70 into passageway 555, an open position thatallows substantially full flow from passageway 70 into passageway 555,and a partially open position positioned at any desired interval betweenthe closed position and the open position and thereby allowing a partialflow, proportional to the amount by which gate 545 is opened, of steam(H₂O) from passageway 70 into passageway 555. Gate 545 may therebyselectively reduce a flow of steam (H₂O) through passageway 70 bydiverting steam (H₂O) through passageway 555.

Gate 550 may be disposed in passageway 555 and may selectively allowflow from passageway 555 into passageway 560 in a manner similar to theoperation of gate 545. Gate 550 may thereby selectively block, partiallyallow, or fully allow flow of steam (H₂O) from passageway 555 intopassageway 560. Passageway 560 may bypass turbine 45 and transfer steam(H₂O) directly to turbine cooling subsystem 60. Therefore, gate 550 maybe operated to selectively allow steam (H₂O) to be directly transferredto turbine cooling subsystem 60 in certain situations such as, forexample, when a rapid shut-down of turbine 45 is desired.

Passageway 555 may be in fluid communication with passageway 565.Passageway 565 may transfer steam (H₂O) from passageway 555 to condenser570. Passageway 565 may pass by an exterior of heat exchanger 20, ratherthan passing through an interior of heat exchanger 20.

Condenser 570 may be disposed in contact with or adjacent to coldreactor coolant passageway 320. Condenser 570 may be any suitablecondenser for condensing steam (H₂O) into water (H₂O). Valve 575 may bedisposed in condenser 570 at any suitable location such as, for example,at a bottom portion of condenser 570. Valve 575 may be any suitablevalve for allowing water (H₂O) to flow out of condenser 570 whilesubstantially blocking a flow of steam (H₂O) out of condenser 570. Forexample, valve 575 may be a float valve. Condenser 570 and valve 575 mayserve as a pressure reduction system, reducing the high pressure of thesteam (H₂O) in passageway 565 to a relatively low pressure of water(H₂O) in passageway 580.

Passageway 580 may be in fluid communication with condenser 570.Passageway 580 may transfer water (H₂O) from condenser 570 to heatexchanger 585. Passageway 580 may pass by an exterior of heat exchanger20, rather than passing through an interior of heat exchanger 20.

Heat exchanger 585 may be any suitable device for facilitating heatexchange from the water (H₂O) transferred through passageway 580. Heatexchanger 585 may be disposed in or near a passageway of turbine steamsubsystem 65 that transfers water (H₂O) from an outlet of H₂O pump 395to heat exchanger 20. Heat exchanger 585 may cool a temperature of thewater (H₂O) to a substantially same temperature as the water (H₂O) beingtransferred by passageway 80 of turbine steam subsystem 65. Passageway590 may transfer water (H₂O) from heat exchanger 585 to passageway 80via junction 595. The water (H₂O) transferred by passageway 590 intopassageway 80 may have a substantially same temperature as thetemperature of water (H₂O) already flowing in passageway 80. Passageway80 may then transfer the water (H₂O) to an inlet of H₂O pump 395 of pumpsubsystem 30.

Bypass subsystem 520 may include a pump 600 and a passageway 605.Passageway 605 may fluidly connect cold reactor coolant passageway 320and hot reactor coolant passageway 325 of transfer subsystem 305. Pump600 may be disposed in passageway 605. Pump 600 may have a relativelysmall capacity such as, for example, between about 2% and about 20% ofthe capacity of pump 390. Pump 600 may operate to pressurize reactorcoolant in passageway 605 to pump reactor coolant from hot reactorcoolant passageway 325 into cold reactor coolant passageway 320, therebybypassing heat exchanger 20 and pump 390. Pump 600 and passageway 605may allow relatively hot reactor coolant flowing through hot reactorcoolant passageway 325 to bypass heat exchanger 20 and flow directlyinto cold reactor coolant passageway 320, thereby allowing hot coolantto mix with the relatively cold coolant and raise the temperature of thecoolant flowing in cold reactor coolant passageway 320. Bypass subsystem520 may operate, for example, during a shut-down and/or initial reactorcoolant loading of nuclear reactor system 5. Bypass system 520 may alsoserve to adjust the effective flow ratios of pumps 390 and 395 (e.g.pump subsystem 30 may be designed to provide the correct ratio ofreactor coolant flow to turbine steam flow at full power, but a slightlydifferent ratio may be desirable at lower power operation).

Moderator stabilization subsystem 525 may include passageways 610, 630,640, and 650, a valve 615, a reservoir 625, a condenser 635, and a pump645, which may be any suitable elements for transferring steam (H₂O) andwater (H₂O).

Passageway 610 may be a relatively large passageway that may fluidlyconnect steam area 110 of reflector zone 95 with reservoir 625. Valve615 may be disposed in passageway 610. Valve 615 may be in a closedposition, substantially blocking flow of steam moderator during normaloperation. When valve 615 is opened, steam moderator may flow intoreservoir 625 via passageway 610. Reservoir 625 may be a low pressurereservoir that may be maintained at a pressure that is less than apressure of steam area 110 of reflector zone 95. Reservoir 625 may be arelatively large and cold storage area. For example, reservoir 625 maybe cooled with a relatively large amount of water (H₂O). For example,reservoir 625 may be cooled with water (H₂O) of turbine steam subsystem65. Upon entering reservoir 625 via passageway 610, the steam moderatormay expand and condense on relatively cold surfaces of interior walls ofreservoir 625. When valve 615 is opened, the rapid flow of moderatorsteam out of steam area 110 of reflector zone 95 may reduce the pressureof the steam moderator in steam area 110 and the pressure of moderatorin reflector zone 95, thus allowing the rapid flow of moderator out ofcontrol cavities 140, 140′, 140 a, and/or 140 b, thereby reducing themass of moderator in the control cavities, reducing the number ofthermal (slow) neutrons available to cause fission, thus leading to arapid shutdown of reactor 15.

Passageway 630 may fluidly connect passageway 610 with condenser 635.Passageway 630 may be a relatively small passageway. For example,passageway 630 may be a pipe that has a significantly smaller diameterthan passageway 610. Passageway 630 may fluidly connect passageway 610to condenser 635. Condenser 635 may be disposed in contact with oradjacent to passageway 80, which may transfer relatively cold water(H₂O), of turbine steam subsystem 65. Condenser 635 may be any suitablecondenser for condensing steam moderator into liquid moderator. Steammoderator transferred from passageway 610 via passageway 630 may becondensed into liquid moderator by condenser 635. Passageway 640 mayfluidly connect condenser 635 with pump 645.

Pump 645 may selectively block a flow of condensed liquid moderator frompassageway 640 into passageway 650. Pump 645 may also selectively allowthe condensed liquid moderator to flow into passageway 650, and mayoperate to pressurize the condensed liquid moderator to flow throughpassageway 650. Passageway 650 may transfer condensed liquid moderatorback into reactor 15. For example, passageway 650 may fluidly connectpassageway 650 with an upper portion of reflector zone 95, e.g., steamarea 110. The condensed liquid moderator transferred into steam area 110via passageway 650 may cause additional steam moderator in steam area110 to condense. Reflector zone 95 may be heated by neutrons escapingfrom reactor core 100, 100′, 100 a, and/or 100 b, and moderator inreflector zone 95 may evaporate into steam moderator in steam area 110.Pump 645 may be operated to condense excess steam moderator from steamarea 110 so as to maintain a stable pressure in steam area 110 andreflector zone 95.

Reactor coolant stabilization subsystem 530 may include a reservoir 655,a heating element 660, and a passageway 665. Reservoir 655 may be apressurized storage tank that may store reactor coolant. Reservoir 655may be supplied with reactor coolant from reactor coolant subsystem 25via passageway 665 from hot reactor coolant passageway 325. Reservoir655 may include liquid reactor coolant in a bottom portion and gaseousreactor coolant at an upper portion. Heating element 660 may selectivelyheat reservoir 655 to maintain the reactor coolant stored withinreservoir 655 at a desired temperature and/or pressure. Heating element660 may be any suitable device for selectively heating reservoir 655such as, for example, an electric heater. Cold reactor coolant from coldreactor coolant passageway 320 may be selectively pumped into reservoir655 by a pump and supply line (not shown) from cold reactor coolantpassageway 320. For example, the pump (not shown) may include aninjector that sprays cold pressurized reactor coolant from cold reactorcoolant passageway 320 into the top (steam) portion of reservoir 655.For example, relatively cold reactor coolant may be sprayed by the pump(not shown) into reservoir 655 to condense a portion of the steamreactor coolant in reservoir 655 to cause some of the steam reactorcoolant to condense and thereby reduce a pressure in reservoir 655 andhot reactor coolant passageway 325.

As illustrated in FIGS. 15 and 20, differential flow subsystem 535 mayinclude a plurality of concentric passageways 670 disposed in a portion675 of cold reactor coolant passageway 320. Concentric passageways 670may replace portion 675 of cold reactor coolant passageway 320, and maybe fluidly connected at both ends of portion 675 to the other portionsof cold reactor coolant passageway 320. Portion 675 may be a risingportion of cold reactor coolant passageway 320 that may be disposeddownstream of pump 390. Any suitable number of concentric passageways670 such as, for example, about ten concentric passageways 670, may bedisposed within cold reactor coolant passageway 320. Concentricpassageways 670 may be, for example, concentric steel pipes. The areabetween concentric passageways may increase, moving from the innermostpassageway 670 to the outermost passageway 670. For example, an area A2between the first and second concentric passageways 670 may be twice aslarge as an area A1 formed within the first concentric passageway 670,an area A3 between the fourth and fifth concentric passageways 670 maybe five times larger than area A1 formed within the first concentricpassageway 670, and an area A4 between the ninth and tenth concentricpassageways 670 may be ten times larger than area A1 formed within thefirst concentric passageway 670. Portions of each area between eachsuccessive concentric passageway 670 may be blocked at each end tomaintain the substantially same flow rate into and out of each of theconcentric passageways 670. Concentric passageways 670 may thereby takea proportionately longer amount of time to transfer the same amount offluid in the outer concentric passageways relative to the innerconcentric passageways, and rapid temperature changes in cold reactorcoolant passageway 320 may therefore be mitigated.

INDUSTRIAL APPLICABILITY

In at least some exemplary embodiments of the disclosed nuclear reactorsystem, a reactor control method may be used having control cavitiesthat enclose a moderator in a core of a reactor. In at least someexemplary embodiments, the moderator in the reactor may be divided intothree areas: a core area that may be disposed anywhere in the reactorless than about 1 foot from any part of a fuel source, a reflector zonethat may include any moderator outside of the core area but less thanthree or four feet from any part of a fuel source, and a moderator poolwhich may include any moderator outside of the core area and reflectorzone. One function of the moderator in the core area is to slow the highspeed neutrons emitted by the fissioning fuel to relatively slow speedsat which the neutrons are much more likely to cause new fissions. Onefunction of the moderator in the reflector zone is to reflect neutronsthat escape from the core area back into the core to decrease the numberof neutrons which are lost from the reactor. The moderator in themoderator pool may have little effect on the reactor (e.g., themoderator may go to the moderator pool when it is displaced from thecore moderator control cavities or may come from the moderator pool whenthe moderator returns to the core). In at least some exemplaryembodiments, the disclosed control cavities may enclose most of themoderator in the reactor core area, and may be closed at the top butallow the free movement of moderator between the bottom of the controlcavity and the reflector and moderator pool areas.

In at least some exemplary embodiments of the disclosed nuclear reactorsystem, when the disclosed nuclear reactor system is producing power ata steady rate, the fuel may be in a state of nuclear equilibrium and thecontrol cavities may be in a state of thermal equilibrium. The twoequilibrium states are coupled by negative feedback such that any changefrom equilibrium in one causes a change in the equilibrium of the other,which will act to counter the change in the first. The disclosed controlcavities are provided with a moderator cooling system that cools thecontrol cavities at about the same rate (or proportional to the volumeof each control cavity if the control cavities are not all the samevolume) by either pumping cool moderator into the control cavities,which mixes with the warmer moderator in the control cavity while anequal mass of the warmer moderator passes out of the control cavity intothe reflector and moderator pool areas, or by passing cooler fluidthrough one or more tubes in the control cavity that then cool thecontrol cavity by conduction. Heat may enter the control cavity bythermal conduction from the hot fuel tubes and by energy deposited inthe moderator by fast neutrons and gamma radiation from the fuel. Whenmore heat enters the control cavity than leaves the control cavity, theliquid moderator in the cavity evaporates and rises into a steam bubbleat the top of the control cavity, while displacing liquid moderator outthe bottom of the control cavity and reducing the total mass ofmoderator in the reactor core because the steam may be much less densethan the liquid moderator. When less heat enters the cavity than isextracted by the moderator cooling system, some of the steam in thesteam bubble condenses, reducing the size of the steam bubble anddrawing liquid moderator into the cavity from the reflector zone andmoderator pool, thereby increasing the total mass of moderator in thecore.

In at least some exemplary embodiments of the disclosed nuclear reactorsystem, high speed neutrons are emitted with each fission of an atom inthe fuel. Most of these high speed neutrons may escape from the fuelinto the moderator (along with gamma radiation emitted by the fuel) andare slowed by collisions with the moderator. These slower neutronsdiffuse from the moderator back into the fuel. There, some of the slowerneutrons may be absorbed by the fissile atoms in the fuel and cause newfissions, some may be absorbed by the fertile atoms in the fuel (e.g.,uranium 238, plutonium 240, and/or thorium 232, if present) and createnew atoms of fissile fuel, and some may be absorbed in the fuel withoutcausing either fission or creation of new fissile atoms or may diffuseback into the moderator. The reaction rate may be stable when, on theaverage, exactly one neutron released by each fission causes a newfission. The probability that a neutron re-entering the fuel from themoderator will cause a fission decreases when the speed is relativelyhigh, and the probability that the neutron will create new fuelincreases when the speed is relatively high. Neutrons leaving themoderator may have a higher average speed when there is less moderatormass in the cavity, and may have a lower average speed when there ismore moderator mass in the cavity. Accordingly, as the steam bubbleincreases in size (and therefore the mass of moderator in the cavitydecreases), the average speed of the neutrons entering the fuelincreases, which increases the number of neutrons that are effectivelydiverted from causing new fissions and decreases the number of neutronsthat are diverted to the production of new fissile fuel. This effectlowers the fission rate, reducing the energy transferred to themoderator, reducing the size of the steam bubble, and thereby providesnegative feedback that maintains a stable size of the steam bubble andmaintains a fission rate that is stable and roughly proportional to themoderator cooling rate.

Collectively, in at least some exemplary embodiments of the disclosednuclear reactor system, the control cavities maintain the total poweroutput stable and proportional to the total moderator cooling rate. Themoderator cooling rate may be controlled by keeping the moderatorcoolant temperature relatively constant and by varying the pumping rateto control the total cooling rate. Individually, each cavity mayinfluence the fission rate of the fuel near it, which causes thereaction rate to be nearly the same at all points in the reactor insteadof higher in the center of the core and lower near the edges of thecore. This may minimize hot spots in the fuel and suppress xenon waves,leading to higher desirable rates of extraction of heat from the fuel.

During normal reactor operation in at least some exemplary embodimentsof the disclosed nuclear reactor system, heat is extracted from the fueltubes by the primary coolant. When the reaction rate is increased, theprimary coolant pumping rate is also increased, so that the temperatureof the fuel tubes does not vary with the reaction rate. Under abnormalconditions, the flow of primary coolant may be insufficient and the fueltubes may become hotter. In such conditions, there may be moreconduction of heat from the fuel tubes into the control cavities, whichmay increase the rate of evaporation of moderator in the controlcavities and increase the size of the steam bubbles in the controlcavities. This may cause liquid moderator to be displaced from thebottom of the cavities, reducing the average density of the moderatorand increasing the average speed of neutrons diffusing from themoderator into the fuel, and thereby decreasing the fission rate.

In at least some exemplary embodiments of the disclosed nuclear reactorsystem, because the steam bubble in the control cavities may be verymuch less dense than the liquid moderator in the control cavities andthe steam bubble may vary in size from substantially non-existent tonearly the size of the entire control cavity, the system may allow theaverage density of the moderator in the core to vary from the fulldensity of the liquid moderator to less than 15% of the full density.This may allow control of the reactor under varying fuel reactivityconditions ranging from enriched new fuel with no xenon load tomoderately-used fuel with an equilibrium xenon load to fuel with a highburnout and consequent high load of neutron absorbing fissionbyproducts. This may be achieved with substantially no loss of neutronsto control absorbers and provide substantially maximum production of newfissile fuel and a substantially maximum fuel conversion ratio at allpoints in the fuel life cycle.

The disclosed nuclear reactor system may be utilized in any applicationusing nuclear-generated power. For example, the disclosed nuclearreactor system may be used in any application using steam (H₂O)generated by using power from a nuclear reaction. The operationdescribed below may generally apply to an operation of all of thedisclosed embodiments of nuclear reactor system 5. Additionally, asdescribed below, some subsystems of the disclosed nuclear reactor systemmay be used in additional applications other than nuclear-generatedpower.

Referring to FIG. 3, an operation of nuclear reactor system 5 may beinitiated when fuel is provided in fuel assembly 125, 125′, 125 a, or125 b having fuel tubes 135, 135′, 135 a, and/or 135 b. When reactor 15is started with fresh fuel in tubes 135, 135′, 135 a, and/or 135 b, thelevel of moderator in control cavity array 130, 130′, 130 a, and/or 135b may stabilize at the equilibrium level based on the reactor design andreactivity of the fuel included in fuel tubes 135, 135′, 135 a, and/or135 b. Over an initial period (e.g., a few days), the levels ofneutron-absorbing xenon-135 and samarium-149 rise to equilibrium levels,and the cooling rate of the moderator may be kept substantially constantby an operation of reactor coolant subsystem 25 (the general operationof reactor coolant subsystem will be described in more detail below).While reactor coolant subsystem 25 is operated to provide a constantrate of cooling of the moderator in control cavity array 130, 130′, 130a, and/or 130 b, the level of xenon and samarium in the fuel will riseand the reactivity of reactor 15 will drop slowly below one, causing thereaction rate to decrease and the energy deposited in the moderator todecrease so that some of the moderator steam condenses. Therefore, moremoderator is drawn into control cavities 140, 140′, 140 a, and/or 140 b,which raises the level of the moderator and the average moderatordensity. This will decrease the number of neutrons undergoing resonancecapture, and thereby compensate for the neutrons that are absorbed bythe gradually increasing amounts of neutron-absorbing xenon and samariumin the fuel of reactor 15. Thus, using control cavity array 130 as anexample, the size of liquid zones 190 and 275 in control cavity array130 may be increased, and the size of gaseous zones 185 and 280 incontrol cavity array 130 may be decreased. A similar effect occurs inthe other disclosed embodiments.

If reactor 15 has a conversion ratio greater than one, or is fueledprimarily with U235 and U238, during steady state operation there may bea period of time during which the reactivity of the fuel may increaseeither because more fissile fuel is created than used or because Pu239is being created from U238 as U235 is burned (because Pu239 is morereactive than U235). If this occurs, the fission rate will rise whilethe cooling remains constant, more neutrons will deposit energy in themoderator, the rate of evaporation in control cavities 140, 140′, 140 a,and/or 140 b will be greater than the rate of condensation, and liquidmoderator will be displaced from control cavities 140, 140′, 140 a,and/or 140 b by the excess steam moderator. This causes less moderationof the neutrons and an increase in the number of neutrons absorbed inthe fertile U238 (or Th232), decreasing the number of thermal neutronsavailable to cause fission and reducing the reaction rate to the ratewhere as much energy is deposited in control cavities 140, 140′, 140 a,and/or 140 b as is removed by reactor coolant subsystem 25. The level ofliquid moderator will decrease gradually as long as the reactivity ofthe fuel continues to rise (e.g., over a period that may last from daysto years). During this period, the fissile content of the fuel mayincrease, and may continue to increase into the next time period(discussed below).

Over the next time period (e.g., the next few months or years), as thefissile content of the fuel is decreased by burnout and the level ofneutron-absorbing fission byproducts rises, the negative feedbackmechanism of control cavities 140, 140′, 140 a, and/or 140 b may operateto cause the level of moderator in control cavity array 130, 130′, 130a, and/or 130 b to rise very slowly to compensate for the reactivity ofthe fuel being decreased by burnout. Eventually, the moderator levelwill rise to the top of control cavity array 130, 130′, 130 a, and/or130 b, and reactor 15 will become subcritical and will stop producingpower. Thus, using control cavity array 130 as an example, there will besubstantially no gaseous zones 185 and 280 in control cavity array 130at this time. A similar effect occurs in the other disclosedembodiments. When reactor 15 stops, the xenon-135 that has been producedthus far by reactor 15 continues to decay, so that in a relatively briefperiod of time (e.g., one or two days), enough xenon-135 will decay sothat reactor 15 can be restarted again. When reactor 15 is restarted,reactor 15 may be run until the concentration of xenon-135 rises againin a relatively short period of time (e.g., a few days). Because thexenon-135 equilibrium concentration changes proportionally to the powerlevel, operation of reactor 15 may continue for relatively longerdurations as the power level of reactor 15 is reduced.

Following the initiation procedure described above, reactor 15 may bemaintained at a steady state operation. In the steady state operation,energy is produced by fission of fuel atoms in fuel tubes 135, 135′, 135a, and/or 135 b. Most of this energy is deposited in the fuel rodsdisposed in the fuel tubes 135, 135′, 135 a, and/or 135 b as heat, whichis extracted from the fuel rods of fuel tubes 135, 135′, 135 a, and/or135 b by a flow of reactor coolant through fuel tubes 135, 135′, 135 a,and/or 135 b that is provided by an operation of reactor coolantsubsystem 25 and pump subsystem 30. Before continuing with thedescription of the steady state operation of reactor 15 and reactor core100, the operation of reactor coolant subsystem 25 and pump subsystem 30will be described.

Referring to FIGS. 2, 3, and 13, transfer subsystem 305 of reactorcoolant subsystem 25 transfers reactor coolant between heat exchanger 20and reactor core 100, 100′, 100 a, or 100 b. Coolant pump 390 of pumpsubsystem 30 may pressurize a flow of reactor coolant in cold reactorcoolant passageway 320 of transfer subsystem 305 to transfer coldreactor coolant from heat exchanger 20 to reactor 15. Cold reactorcoolant flowing in passageway 320 may thereby flow through apertures ofcontainment structure 85 and into reflector zone 95.

The cold reactor coolant flowing in cold reactor coolant passageway 320may flow into passageways 330 of fuel coolant subsystem 310. The coldreactor coolant flowing in passageways 330 passes through fuel tubes135, 135′, 135 a, and/or 135 b to facilitate heat exchange with fueltubes 135, 135′, 135 a, and/or 135 b. Fuel tubes 135, 135′, 135 a,and/or 135 b impart heat via heat transfer to the cold reactor coolantflowing through passageways 330, thereby turning the cold reactorcoolant into hot reactor coolant. Thus, the reactor coolant leaves fueltubes 135, 135′, 135 a, and/or 135 b with more energy per pound than thereactor coolant had when entering fuel tubes 135, 135′, 135 a, and/or135 b, either by increasing the temperature of the reactor coolant or bychanging the reactor coolant from a liquid to a gaseous state, or both.Passageways 330 may then transfer the hot reactor coolant to hot reactorcoolant passageway 325 of transfer subsystem 305.

In the first described embodiment, some of the cold reactor coolantflowing in cold reactor coolant passageways 330 also flows intopassageways 335 of moderator coolant subsystem 315. The cold reactorcoolant flowing in passageways 335 passes through control cavities 140to facilitate heat exchange with control cavities 140. The cold reactorcoolant flowing in passageway 335 is heated somewhat by heat exchange bymoderator confined within control cavities 140, and is transferred outof control cavities 140 via passageways 335 and back into passageways330. The cold reactor coolant flowing in passageways 330 passes throughreflecting pool 105. The cold reactor coolant flowing throughpassageways 330 is heated somewhat by heat exchange by the moderator ofreflecting pool 105. The reactor coolant flowing in passageways 330 maythen pass through fuel tubes 135 and thereby be heated from cold reactorcoolant into hot reactor coolant. Passageways 330 may then transfer thehot reactor coolant to hot reactor coolant passageway 325 of transfersubsystem 305.

The reactor coolant flowing through passageway 335 of moderator coolantsubsystem 315 may flow, for example, in the arrangement depicted in FIG.14. Reactor coolant from cold reactor coolant passageway 320 of transfersubsystem 305 may flow into passageway 335 via intermediate passageway330 and entry member 350. Reactor coolant then flows through channel 380of interior member 355. Some of the reactor coolant may flow along afull length of channel 380 until reaching end portion 370. However, someof the reactor coolant may also flow directly from channel 380 intochannel 385, via apertures 375, before reaching end portion 370. Becausesome of the relatively cold reactor coolant passes directly into channel385 via apertures 375, and mixes with the relatively hot reactor coolantin channel 385, a temperature of the reactor coolant in channel 385 mayremain relatively constant along the length of passageway 335. Sizesand/or spacings of apertures 375 may be designed to maximize themaintenance of a generally constant temperature in channel 385. Forexample, the amount of mixing of reactor coolant between channels 380and 385 may increase in a direction moving toward end portion 370. Thereactor coolant then flows through channel 385, and back into reactorcoolant passageway 330 of transfer subsystem 305, via exit member 365.

Coolant pump 390 of pump subsystem 30 may pressurize a flow of coldreactor coolant in cold reactor coolant passageway 320 of transfersubsystem 305 through the fuel tubes 135, and a flow of hot reactorcoolant from reactor 15 back to heat exchanger 20 via hot reactorcoolant passageway 325.

Fission of the fuel in fuel tubes 135, 135′, 135 a, and/or 135 bproduces energetic higher speed neutrons (e.g., neutrons traveling at arelatively intermediate or high speed). These energetic higher speedneutrons deposit energy in the moderator of control cavity array 130,130′, 130 a, and/or 130 b by colliding with moderator atoms. Theenergetic higher speed neutrons are slowed to a low energy state (“slowneutrons”) by these collisions with moderator atoms, and some of theslow neutrons then cause fission of the fuel atoms. The reactor may beconsidered stable (e.g., at a constant power production) when, for eachfission of a fuel atom, one of the neutrons produced causes a newfission. Thus, the reactor may be considered stable when, on average,exactly one of the neutrons produced by the fission of a fuel atomcauses a new fission.

As the moderator in control cavity array 130, 130′, 130 a, and/or 130 bis heated by energetic neutrons, some of the moderator may evaporateinto steam moderator (e.g., boil into a gaseous state). Steam moderatorin the gaseous state is less dense than liquid moderator (e.g., in aliquid state) and will rise to the upper portion of control cavities140, 140′, 140 a, and/or 140 b in which it is confined because controlcavities 140, 140′, 140 a, and/or 140 b are closed at an upper portionand may therefore confine the moderator at an upper portion. Because thevolumes of control cavities 140, 140′, 140 a, and/or 140 b may beconstant, low density gaseous steam moderator that is confined and thataccumulates in upper portions of control cavities 140, 140′, 140 a,and/or 140 b will displace higher density liquid moderator out of thelower portions of control cavities 140, 140′, 140 a, and/or 140 b. Thus,the overall average density of the moderator in control cavities 140,140′, 140 a, and/or 140 b is reduced. To keep substantially all of themoderator in control cavities 140, 140′, and 140 a from turning intosteam moderator, control cavities 140, 140′, 140 a, and/or 140 b arecooled by reactor coolant subsystem 25. Reactor coolant subsystem 25 maycause some of the gaseous steam moderator to condense into the denserliquid moderator. Less steam moderator will therefore be confined in theupper portions of control cavities 140, 140′, 140 a, and or 140 b, soless relatively high density liquid moderator will be displaced out ofcontrol cavities 140, 140′, 140 a, and/or 140 b. Accordingly, liquidmoderator will flow back into control cavities 140, 140′, 140 a, and/or140 b through the open lower portions and/or side portions of controlcavities 140, 140′, 140 a, and/or 140 b.

Referring to FIGS. 7 and 8 and using control cavity array 130 as anexample, reactor coolant subsystem 25 may remove less energy by heattransfer from the moderator confined in control cavity array 130.Accordingly, an increasing amount of moderator will be heated byenergetic neutrons into steam moderator. Thus, as an increasing amountof steam moderator is confined and accumulates in upper portions ofcontrol cavities 140, boundary 195 will drop as an increasing amount ofliquid moderator is displaced out of control cavities 140 (e.g.,displaced under intermediate member 170 and end member 165). Thus,gaseous zone 185 will increase in size, and liquid zones 190 willdecrease in size. Similarly in cone assembly 150, as reactor coolantsubsystem 25 removes less energy by heat transfer, an increasing amountof steam moderator is confined and accumulates in upper portions ofinner cone assemblies 200 and outer cone assemblies 205. Thus, boundary290 will drop as an increasing amount of liquid moderator is displacedout of inner cone assemblies 200 and outer cone assemblies 205 (e.g.,displaced under interior cone 235 and exterior cone 240). Thus, gaseouszone 280 will increase in size, and liquid zones 190 and 275 willdecrease in size. A similar effect occurs in the other disclosedembodiments of reactor 15.

The converse effect also occurs. Again using control cavity array 130 asan example, reactor coolant subsystem 25 may remove more energy by heattransfer from the moderator confined in control cavity array 130.Accordingly, a decreasing amount of moderator will be heated byenergetic neutrons into steam moderator. Thus, as a decreasing amount ofsteam moderator is confined and accumulates in upper portions of controlcavities 140, boundary 195 will rise as liquid moderator re-enterscontrol cavities 140 (e.g., re-enters under intermediate member 170 andend member 165). Thus, gaseous zone 185 will decrease in size, andliquid zone 190 will increase in size. Similarly in cone assembly 150,as reactor coolant subsystem 25 removes more energy by heat transfer, adecreasing amount of steam moderator is confined and accumulates inupper portions of inner cone assemblies 200 and outer cone assemblies205. Thus, boundary 290 will rise as an increasing amount of liquidmoderator re-enters inner cone assemblies 200 and outer cone assemblies205 (e.g., re-enters under interior cone 235 and exterior cone 240).Thus, gaseous zone 280 will decrease in size, and liquid zones 190 and275 will increase in size. Steam moderator may also condense along thesides of control cavities 140 and drip back into liquid zones 190 and275. A similar effect occurs in the other disclosed embodiments ofreactor 15.

When reactor coolant subsystem 25 operates to extract substantially asmuch energy from control cavity arrays 130, 130′, 130 a, and/or 130 b asis deposited from the fuel in fuel tubes 135, 135′, 135 a, and/or 135 b,the rate of evaporation and the rate of condensation in control cavities140, 140′, 140 a, and/or 140 b will be substantially equal, and the sizeof gaseous zones 185, 185′, 185 a, 280, and/or 185 b will remainsubstantially constant. Thus, there will be substantially no movement ofmoderator into or out of control cavities 140, 140′, 140 a, and/or 140b.

The higher speed neutrons may be slowed by collisions with moderatoratoms when the moderator atoms are either in the liquid state (liquidmoderator) or the gaseous state (steam moderator). When the averagedensity of the moderator is decreased (e.g., by increasing a size ofgaseous zones 185, 185′, 185 a, 280, and/or 185 b), an average distancebetween moderator atoms is increased and an average distance that theneutrons must travel between collisions is increased. When the higherspeed neutrons travel further between each collision they spend moretime at the higher speeds and so the average number of neutronstraveling at relatively high and intermediate speeds is greater. Whileslow neutrons may have a relatively high probability of causing fissionwhen they collide with fuel atoms disposed in fuel tubes 135, 135′, 135a, and/or 135 b, higher speed neutrons may have a relatively higherprobability of being absorbed within reactor 15 without causing fission.Accordingly, the number of slow neutrons available to cause fission willdecrease.

When reactor 15 operates at a steady state operation level, reactorcoolant subsystem 25 may operate to maintain gaseous zones 185, 185′,185 a, 280, and/or 185 b at a desired substantially constant size. Thisdesired size of gaseous zones 185, 185′, 185 a, 280, and/or 185 b mayprovide a desired density of moderator within control cavity array 130,130′, 130 a, and/or 130 b so that just enough higher speed neutrons willbe absorbed at intermediate and high speeds so that there are a desiredamount of remaining slow neutrons traveling at relatively slow speeds tocause one new fission for each old fission in fuel assemblies 125, 125′,125 a and 125 b.

Gaseous zones 185, 185′, 185 a, 280, and/or 185 b may be maintained at adesired substantially constant size by using negative feedback. Asdescribed above, reactor coolant subsystem 25 may be controlled tosubstantially match the cooling rate of reactor core 100, 100′, 100 aand 100 b (e.g., by controlling the flow of coolant through controlcavity arrays 130, 130′, 130 a, and/or 130 b) with the fission rate (andthereby the heating rate of heat imparted into moderator in controlcavity arrays 130, 130′, 130 a, and/or 130 b by fission in fuelassemblies 125, 125′, 125 a and 125 b) of reactor core 100, 100′, 100 aand 100 b. If the heating rate of heat imparted into control cavityarrays 130, 130′, 130 a, and 130 b by fission in fuel assembly 125,125′, 125 a and 125 b is higher than the cooling rate provided byreactor coolant subsystem 25, gaseous zones 185, 185′, 185 a, 280,and/or 185 b will expand. The expansion of gaseous zones 185, 185′, 185a, 280, and/or 185 b decreases the average density of the moderator incontrol cavity arrays 130, 130′, 130 a, and/or 130 b, which increasesthe percentage of neutrons lost by absorption at intermediate and highspeeds (resonance capture), thus decreasing the percentage of slowneutrons available to cause fission, which decreases the heating rate ofreactor 15. If the heating rate is lower than the cooling rate, gaseouszones 185, 185′, 185 a, 280, and/or 185 b will shrink, increasing theaverage density of the moderator in control cavity arrays 130, 130′, 130a, and/or 130 b, decreasing the percentage of neutrons lost by resonancecapture, thus increasing the percentage of slow neutrons available tocause fission, which increases the heating rate. Thus, reactor 15 iscontrolled to cause the reaction rate to follow the cooling rate ofcontrol cavity array 130, 130′, 130 a, and/or 130 b by reactor coolantsubsystem 25. Accordingly, increasing or decreasing the cooling rate ofcontrol cavity array 130, 130′, 130 a, and/or 130 b will cause acorresponding increase or decrease in the total power output of reactor15. Because the amount of energy deposited in the moderator may be onlya small percentage (e.g., between about 1% and about 5%, such as, forexample, about 3%) of the total energy produced by reactor 15, only arelatively small amount of energy (and corresponding heat) of the totalenergy produced by reactor 15 is adjusted by a relatively small coolingrate (relative to the total energy produced by reactor 15) to maintaincontrol of reactor 15. Thus, controlling a relatively small cooling rateallows simple and stable control of a total power output of reactor 15that is, for example, about 30 times greater than the amount of heat andenergy that is imparted to the moderator (and that is controlled byadjusting the cooling rate).

Solely to illustrate a comparison between a relatively large total poweroutput of reactor 15 and the relatively small amount of energy impartedto a moderator, an example of a reactor for powering a 1000 Megawattelectric power generator may be considered. The total energy produced bythe exemplary power generator may be about 10,000,000,000 BTU/hour whenthe generator is running at full power. If the moderator is heavy water(D₂O) at a temperature of around 540 degrees Fahrenheit, the reactorcore may contain, for example, around 100 tons of moderator. Assumingthat 3% of the total energy produced by the reactor is deposited in thecore moderator, then the amount of energy imparted to the moderator maybe around 300,000,000 BTU/hour or 1,500 BTU/hour per pound of moderator.At this rate, even if there were no cooling provided, it may take about25 minutes to boil away each pound of moderator. Because gaseous steammoderator may be about 20 times less dense than liquid moderator at thisexemplary temperature, it may take about a minute to boil enoughmoderator to displace the remainder of the pound of liquid moderatorfrom control cavities 140, 140′, 140 a, and/or 140 b in this example.This example is purely provided to show the relative amount of energyimparted to moderator. The disclosed method and apparatus may be used inany type or size of nuclear reactor system.

Reactor 15 may provide energy from a nuclear reaction to powergeneration subsystem 10 at any suitable time during its operation. Anexample of how reactor 15 powers power generation subsystem 10 will nowbe provided, using steady state operation as an illustrative example.Reactor 15 may also similarly power generation subsystem 10 during otherphases and operation states of nuclear reactor system 5.

Referring to FIGS. 1 and 13, coolant pump 390 pressurizes a flow ofreactor coolant through cold reactant cooler passageway 320 and hotreactor coolant passageway 325 of reactor coolant subsystem 25. Reactorcoolant subsystem 25 thereby transports hot reactor coolant to the steamgenerators disposed in heat exchanger 20 via hot reactor coolantpassageway 325. The hot reactor coolant flowing through the steamgenerator tubes boils water (H₂O), which was delivered to heat exchanger20 by turbine steam subsystem 65 (as explained further below), via heattransfer. While passing through heat exchanger 20, reactor coolantflowing through hot reactor coolant passageway 325 is cooled throughheat transfer between the reactor coolant and water (H₂O) in heatexchanger 20. The cooled reactor coolant is then subsequently returnedto reactor 15 via cold reactant coolant passageway 320 of reactorcoolant subsystem 25. Reactor coolant subsystem 25 continuously repeatsthis cycle, transferring a desired amount of hot reactor coolant, whichhas been heated by reactor 15, to heat exchanger 20 and thensubsequently returning the cooled reactor coolant to reactor 15. Thehigh pressure steam (H₂O) generated by the steam generators of heatexchanger 20 is then transferred to turbine 45 via passageway 70 ofturbine steam subsystem 65 (of power generation subsystem 10), based ona flow of steam (H₂O) and water (H₂O) produced by H₂O pump 395. H₂O pump395 pressurizes a flow of steam (H₂O) and water (H₂O) in heat exchanger20, passageway 70, passageways of turbine 45, passageway 75, turbinecooling subsystem 60, and passageway 80.

Turbine 45 converts the high pressure steam (H₂O) that is delivered bypassageway 70 of turbine steam subsystem 65 into mechanical energy. Forexample, the steam (H₂O) urges the plurality of elements mounted on theexemplary rotatable shaft of turbine 45 described above, and expandsthrough the series of exemplary cylinders described above to drive theshaft of turbine 45. This operation of turbine 45 merely illustrates oneof any suitable methods for producing mechanical energy from steam(H₂O). The mechanical energy of the exemplary shaft of turbine 45 isthen mechanically transferred to drive assembly 50 of power generationsubsystem 10.

Drive assembly 50 then mechanically transfers the imparted mechanicalenergy to generator 55 of power generation subsystem 10 via theexemplary driveshaft assembly described above or via any other suitablemechanical connection. Drive assembly 50 may thereby drive generator 55to produce electricity. As one example, generator 55 generates ACelectricity at any suitable frequency such as, for example, 50 Hz (50cycle) or 60 Hz (60 cycle) power. The electricity from generator 55 isthen provided via conventional transfer techniques to a power grid orany other site or activity that uses electricity.

Passageway 75 of turbine steam subsystem 65 transfers surplus or deadsteam (H₂O) from turbine 45 to turbine cooling subsystem 60 of powergeneration subsystem 10. Turbine cooling subsystem 60 uses any suitabletechnique such as, for example, using condensers, cooling towers, forcedairflow, and/or once-through cooling to condense steam (H₂O) into water(H₂O). The relatively cold water (H₂O) is then transferred from turbinecooling subsystem 60 to heat exchanger 20 via passageway 80.

The relatively cold water (H₂O) delivered to heat exchanger 20 viapassageway 80 of turbine steam subsystem 65 enters heat exchanger 20.Some of the relatively cold water (H₂O) enters the lower interiorportion of heat exchanger 20 and some of the relatively cold water (H₂O)enters heat exchanger 20 at the central and/or upper portion of heatexchanger 20. The relatively cold water (H₂O) entering the lowerinterior portion is heated and is boiled by heat transfer with the hotreactor coolant transferred into heat exchanger 20 via hot reactorcoolant passageway 325 of reactor coolant subsystem 25. The relativelycold water (H₂O) entering at the upper portion is injected into thelower interior portion of heat exchanger 20 via the plurality of nozzles83 disposed at the central and/or upper portion of heat exchanger 20, oninterior walls of heat exchanger 20. The plurality of nozzles 83 injectthe water (H₂O) into the boiling water (H₂O) already contained withinthe interior portion of heat exchanger 20. The relatively cold water(H₂O) mixes with the boiling water (H₂O) to help reduce the magnitude ofthe temperature gradient of H₂O contained inside heat exchanger 20. Theabove exemplary illustration of transfer of water (H₂O) to heatexchanger 20 is provided merely as an example, and any suitable knowntechnique for heat exchange may be used in heat exchanger 20.

The above-described process of using energy from a nuclear reaction inreactor 15 to produce steam (H₂O) in heat exchanger 20, using the steam(H₂O) to drive turbine 45, and driving generator 55 by turbine 45 iscontinuously repeated to produce a desired amount of electricity.Similarly, the process of condensing steam (H₂O) into water (H₂O) andreturning the water (H₂O) to heat exchanger 20 is continuously repeatedas desired. Thus, this process is repeated continuously as desired asreactor 15 powers power generation subsystem 10 to produce energy suchas, for example, electricity.

As nuclear reactor system is operated in a steady state operation, powerdemands may fluctuate. Power demands may fluctuate on a daily basis.Depending on the time of the day or during the night, average powerdemands may change (e.g., power demands may be lower in the middle ofthe night on a weeknight as compared with during a weekday morning or anight during the weekend). Controller 540 of reactor control subsystem40 may be operated to vary a power output of nuclear reactor system 5.Controller 540 may be operated to control reactor control subsystem 40and pump subsystem 30 to vary a cooling rate of reactor coolant and ormoderator coolant in reactor 15, thereby varying a power output ofnuclear reactor system 5 by using negative feedback.

When it is desired for nuclear reactor system 5 to generate a greateramount of power, controller 540 is operated to control reactor controlsubsystem 40 and pump subsystem 30 to increase a cooling rate ofmoderator in reactor 15 so that the cooling rate of moderator is greaterthan the heating rate of the moderator by fuel tubes 135, 135′, 135 a,and/or 135 b. Controller 540 controls coolant pump 390 to cause arelatively greater amount of reactor coolant to flow through reactor 15.If the cooling rate provided by reactor coolant subsystem 25 to themoderator in control cavity arrays 130, 130′, 130 a, and/or 130 b isgreater than the heating rate of heat imparted into moderator in controlcavity array 130, 130′, 130 a, and/or 130 b by fission in fuel assembly125, 125′, and 125 a, gaseous zones 185, 185′, 185 a, 280, and/or 185 bwill shrink. The shrinking of gaseous zones 185, 185′, 185 a, 280,and/or 185 b increases the average density of the moderator in controlcavity arrays 130, 130′, 130 a, and/or 130 b, which decreases thepercentage of neutrons lost by resonance capture, thus increasing thepercentage of slow neutrons available to cause fission, and increasingthe heating rate of reactor 15. By increasing the heating rate ofreactor 15, a greater amount of heat will be imparted into the reactorcoolant flowing in hot reactor coolant passageway 325, and a greateramount of heat will therefore be transferred by reactor coolantsubsystem 25 into heat exchanger 20. Heat exchanger 20 will therebyproduce a greater amount of steam (H₂O), and a greater amount of steam(H₂O) will be transferred from heat exchanger 20 to turbine 45 viapassageway 70. Controller 540 is also operated to cause H₂O pump 395 tocause a greater flow of steam (H₂O) to be transferred to turbine 45. Thegreater amount of steam (H₂O) will cause turbine 45 to produce a greateramount of mechanical energy, which when transferred from turbine 45 togenerator 55 via drive assembly 50, will cause generator 55 to produce arelatively greater amount of power (e.g., electricity).

When it is desired for nuclear reactor system 5 to generate a lesseramount of power, controller 540 is operated to control reactor controlsubsystem 40 and pump subsystem 30 to decrease a cooling rate ofmoderator in reactor 15 so that the cooling rate of moderator is lessthan the heating rate of the moderator by fuel tubes 135, 135′, 135 a,and/or 135 b. Controller 540 controls coolant pump 390 to cause arelatively lesser amount of reactor coolant to flow through reactor 15.If the cooling rate provided by reactor coolant subsystem 25 to themoderator in control cavity arrays 130, 130′, 130 a, and/or 130 b isless than the heating rate of heat imparted into moderator in controlcavity array 130, 130′, 130 a, and/or 130 b by fission in fuel assembly125, 125′, and 125 a, gaseous zones 185, 185′, 185 a, 280, and/or 185 bwill expand. The expansion of gaseous zones 185, 185′, 185 a, 280,and/or 185 b decreases the average density of the moderator in controlcavity arrays 130, 130′, 130 a, and/or 130 b, which increases thepercentage of neutrons lost by resonance capture, thus decreasing thepercentage of slow neutrons available to cause fission, and decreasingthe heating rate of reactor 15. By decreasing the heating rate ofreactor 15, a lesser amount of heat will be imparted into the reactorcoolant flowing in hot reactor coolant passageway 325, and a lesseramount of heat will therefore be transferred by reactor coolantsubsystem 25 into heat exchanger 20. Heat exchanger 20 will therebyproduce a lesser amount of steam (H₂O), and a lesser amount of steam(H₂O) will be transferred from heat exchanger 20 to turbine 45 viapassageway 70. Controller 540 is also operated to cause H₂O pump 395 tocause a lesser flow of steam (H₂O) to be transferred to turbine 45. Thelesser amount of steam (H₂O) will cause turbine 45 to produce a lesseramount of mechanical energy, which when transferred from turbine 45 togenerator 55 via drive assembly 50, will cause generator 55 to produce arelatively lesser amount of power (e.g., electricity).

The shrinking and/or expansion of gaseous zones 185, 185′, 185 a, 280,and/or 185 b may be very gradual and/or slight and still providesufficient control of nuclear reactor system 5. So, even a small changein the volume of gaseous zones 185, 185′, 185 a, 280, and/or 185 b mayprovide a large enough difference to affect resonance capture and tosufficiently control reactor 15 by negative feedback.

The operation of reactor core 100 b may generally follow the operationof reactor cores 100, 100′, and 100 a described above. As depicted inFIGS. 12I, 12J, and 12K, reactor 100 b provides additional features forconfining moderator in control cavity array 130 b that may be used with,for example, a higher percentage of fast fission.

As illustrated in FIGS. 12I, 12J, and 12K, relatively cool moderator isfree to move from reflecting pool 105 and into moderator coolant inflowtube 335 b. Moderator disposed in moderator coolant inflow tube 335 b isthen free to move into control cavities 140 b via holes 336 b, therebycooling moderator in control cavities 140 b. A substantially equalvolume of warmer moderator moves out of control cavity 140 b and intomoderator outflow tube 337 b via holes 338 b. Moderator in moderatoroutflow tube 337 b is free to move from moderator outflow tube 337 binto reflector zone 95. Because control cavities 140 b have closed upperportions, moderator may not be free to move between the upper portionsof control cavities 140 b and reflector zone 95.

Referring to FIG. 12N, the disclosed embodiment may operate when, forexample, moderator is cooled by circulation of relatively cool moderatorthrough and into reflecting pool 105 and/or control cavity 140 b (and/or140′ and/or 140 a). The embodiment of FIG. 12N may operate based on thestability of the pressure of steam moderator at substantially all pointsin the system, and stability of the height of boundary 115 disposed atthe top of reflecting pool 105 above fuel rods 127 b (and/or similarfuel rods disposed in reactor core 100′ and 100 a). Moderator coolanttube 327 b (and/or similar moderator coolant tubes disposed in reactorcore 100′ and 100 a) allows the flow of moderator from reflector zone 95and control cavities 140 b (and/or control cavities 140′ and/or 140 a)into moderator heat exchange tubes 390 b that pass through tank 377 b topassageway 355 b and moderator coolant pump 350 b. The moderator coolingrate may be, for example, the pump flow rate multiplied by thedifference in temperature between the water (H₂O) temperature in tank377 b and the moderator temperature in reflecting pool 105. Because thetemperature difference may be maintained at a constant level, themoderator control cavity cooling rate and thus the reactor total poweroutput are proportional to the pump flow rate. Thus, an improperoperation of moderator coolant pump 350 b and/or a disruption of pumppower will shut down the reaction in reactor 15. The cooled moderatorflows from moderator coolant pump 350 b via passageway 322 b (and/orsimilar passageway disposed in reactor cores 100′ and/or 100 a) tomoderator coolant inflow tubes 335 b (and/or similar tubes disposed inreactor cores 100′ and/or 100 a). A condenser and differential flowportion similar in form and function to condenser 570 and differentialflow portion 675 of load-following subsystem 515 may be inserted intopassageway 322 b adjacent to pump 350 b.

The operation of reactor control subsystem 40 will now be described,beginning with a description of an exemplary operation of load-followingsubsystem 515. The operation of reactor control subsystem is controlledvia controller 540 of control subsystem 510.

As illustrated in FIG. 20, gate 545 of load-following subsystem 515selectively reduces a flow of steam (H₂O) from heat exchanger 20 toturbine 45 via passageway 70 by diverting steam (H₂O) from passageway 70into passageway 555. To divert steam (H₂O) into passageway 555, gate 545is moved from the closed position to the partially open position or thefully open position. When gate 545 is in the closed position,substantially all of the flow of steam (H₂O) flows from passageway 70 toturbine 45. When gate 545 is moved to the partially open position, (e.g.when the desired flow of steam to turbine 45 must decrease to meet alower electrical power demand) the excess steam (H₂O), which isproportional to the amount by which gate 545 is opened, flows frompassageway 70 into passageway 555. Thus, the operation of gate 545controls the amount of steam (H₂O) that is diverted from passageway 70into passageway 555. An operation of gate 550, which is similar to theoperation of gate 545, controls an amount steam (H₂O) that is divertedfrom passageway 555 into passageway 560. Steam (H₂O) that flows intopassageway 560 is transferred directly to turbine cooling subsystem 60via passageway 560. Thus, an operation of gate 550 controls the amountof flow of steam (H₂O) that bypasses turbine 45 and is transferreddirectly to turbine cooling subsystem 60. Depending on its position, andoperating similarly to gate 545, gate 550 may divert substantially allflow, substantially no flow, or some flow of steam (H₂O) from passageway555 to turbine cooling subsystem 60 via passageway 560. When a rapidshut-down of turbine 45 is desired, gate 545 is moved to the openposition to transfer substantially all flow of steam (H₂O) frompassageway 70 into passageway 555, and gate 550 is moved to the openposition to transfer substantially all flow of steam (H₂O) frompassageway 555 into passageway 560. Thus, substantially all flow ofsteam (H₂O) from heat exchanger 20 is diverted to turbine coolingsubsystem 60, facilitating the rapid shut-down of turbine 45.

The steam (H₂O) flowing through passageway 555, which is not diverted toturbine cooling subsystem 60 via passageway 560, flows to condenser 570via passageway 565 or may flow to a similar condenser (not shown) inpassageway 322 b, as depicted in FIG. 12N. Because of heat exchangebetween the steam (H₂O) disposed in condenser 570 and cold reactorcoolant flowing through cold reactor coolant passageway 320, some orsubstantially all of the steam (H₂O) disposed in condenser 570 condensesinto water (H₂O). Valve 575 operates to allow water (H₂O) to flow out ofcondenser 570 while substantially blocking a flow of steam (H₂O) out ofcondenser 570. Water (H₂O) then flows from condenser 570 to heatexchanger 585 via passageway 580. Heat exchanger 585 cools a temperatureof the water (H₂O) to a desired temperature (e.g., a substantially sametemperature as the water (H₂O) being transferred by passageway 80 ofturbine steam subsystem 65). Passageway 590 then transfers water (H₂O)from heat exchanger 585 to passageway 80 via junction 595. Passageway 80then transfers the water (H₂O) to an inlet of pump 395 of pump subsystem30.

Therefore, load-following subsystem 515 allows control of turbine 45 byadjusting gate 545 to direct more or less of the steam (H₂O) from heatexchanger 20 to pass through turbine 45 as power demand fluctuates. Insome cases of normal operation, the excess steam (H₂O) is used topre-heat the input feedstock from turbine cooling subsystem 60 to heatexchanger 20. Also, some of the excess steam (H₂O) may be used to heatprimary moderator control cavity coolant via a heat exchanger (e.g., asmall heat exchanger) disposed in passageway 322 b or passageway 320,thus reducing the cooling of control cavities 140, 140′, 140 a, and/or140 b and the reactor power output when the amount of excess steam (H₂O)increases (or increasing the power output when the amount of excesssteam (H₂O) decreases).

An exemplary operation of bypass subsystem 520 will now be described.Pump 600 is controlled by controller 540 to selectively pressurizereactor coolant in passageway 605 to pump reactor coolant from hotreactor coolant passageway 325 into cold reactor coolant passageway 320,thereby bypassing heat exchanger 20 and pump 390. Thus, pump 600 andpassageway 605 allow relatively hot reactor coolant flowing through hotreactor coolant passageway 325 to bypass heat exchanger 20 and flowdirectly into cold reactor coolant passageway 320, thereby allowing hotcoolant to mix with the relatively cold coolant and raise thetemperature of the coolant flowing in cold reactor coolant passageway320 at desired times during operation of reactor 15 (e.g., during ashut-down, low power operation, and/or initial reactor coolant loading).

Therefore, bypass subsystem 520 allows a relatively small amount ofprimary coolant to be forced from the normal coolant path, bypassingheat exchanger 20 and/or reactor core 100, 100′, 100 a, and/or 100 b.Bypass subsystem 520 may operate when coolant pump 390 and/or H₂O pump395 are driven by a single motor, and proportional amounts of fluid arepumped through transfer subsystem 305 to balance the amount of heatentering heat exchanger 20 via the hot reactor coolant passageway 325and the amount of heat leaving heat exchanger 20 via steam (H₂O) flowthrough passageway 70 to turbine 45 during normal operation. At lowpower, significant temperature deviations may occur (e.g., largertemperature deviations than at full power), and these temperaturedeviations may change the flow ratio between a primary coolant flow ratethrough hot reactor coolant passageway 325 and a turbine feedstock flowrate through passageway 70 away from a desired flow ratio. The operationof bypass subsystem 520 compensates for these temperature deviations andmaintains the flow ratio between a primary coolant flow rate through hotreactor coolant passageway 325 and a turbine feedstock flow rate throughpassageway 70 at a desired flow ratio. In responding to thesetemperature deviations, pump 600 may operate at a relatively lowcapacity. For example, the capacity of pump 600 may be 3% of thecapacity of pump 390 at full power, which may correspond to 30% of thecapacity of pump 390 at 10% power, which may be enough capacity for pump600 to compensate for a significant imbalance in desired flow ratio.Pump 600 may also operate in situations when it is not desirable to runany turbine feedstock through passageway 70 to turbine 45, but it isdesirable to maintain a small flow of primary reactor coolant throughreactor core 100, 100′, 100 a, and/or 100 b (e.g., at reactor startup tobring reactor core 100, 100′, 100 a, and/or 100 b uniformly up tooperating temperature).

An exemplary operation of moderator stabilization subsystem 525 will nowbe described. During normal operation of reactor 15, valve 615 is in aclosed position, substantially blocking flow of steam moderator fromsteam area 110 of reflector zone 95 into reservoir 625 via passageway610. When controller 540 controls valve 615 to open, steam moderatorflows from steam area 110 into reservoir 625 via passageway 610. Uponentering reservoir 625 via passageway 610, the steam moderator condenseson relatively cold surfaces of interior walls of reservoir 625. Valve615 may be open when a rapid shutdown of the reactor is desired. Steammoderator flowing through passage 610 also flows into condenser 635 viapassageway 630. Because of heat exchange with relatively cold water(H₂O) flowing through passageway 80, steam moderator disposed incondenser 635 condenses into liquid moderator. Pump 645 selectivelypressurizes a flow of liquid moderator in passageways 640 and 650,thereby pumping condensed liquid moderator back into reactor 15, e.g.,into steam area 110. The condensed liquid moderator transferred intosteam area 110 via passageway 650 causes additional steam moderator insteam area 110 to condense, and reduces a temperature of moderator inreflector zone 95. Pump 645 may be operated at a flow rate thatmaintains a constant steam pressure in steam area 110 and reflector zone95. This function is also served by steam pressure control valve 380 b,depicted in FIG. 12N.

Therefore, moderator stabilization subsystem 525 operates to condenseexcess steam moderator and pump it back into reflecting pool 105 when apressure of the steam moderator in steam area 110 rises above a desiredvalue. Maintaining the pressure of steam moderator in steam area 110 ata desired pressure range provides for a normal operation of controlcavities 140, 140′, 140 a, and/or 140 b, because moderator stabilizationsubsystem 525 operates to maintain stability of the steam pressure insteam zone 110, to maintain stability of a temperature of the steammoderator near boundary 115 of reflector zone 95, and to maintainstability of a temperature of liquid moderator near boundary 115 ofreflector zone 95.

An exemplary operation of reactor coolant stabilization subsystem 530will now be described. Substantially free passage of reactor coolantbetween reservoir 655 and hot reactor coolant passageway 325 occurs viapassageway 665. Heating element 660 selectively heats reservoir 655 tomaintain the reactor coolant stored within reservoir 655 at a desiredtemperature and/or pressure when the pressure drops below the desiredvalue. When the pressure rises above a desired value, cold reactorcoolant from cold reactor coolant passageway 320 is selectively injectedinto reservoir 655 by a pump (not shown). The relatively cold reactorcoolant sprayed into reservoir 655 condenses a portion of the steamreactor coolant in reservoir 655, thereby selectively reducing apressure in reservoir 655 and hot reactor coolant passageway 325.

Referring to FIGS. 15 and 20, an exemplary operation of differentialflow subsystem 535 will now be described. Because portions of each area(e.g., area A1, A2, A3, and/or A4) at the entry and exit ends of eachsuccessive concentric passageway 670 may be blocked, a substantiallysame flow rate in each of the concentric passageways 670 is maintainedthrough the portions of cold reactor coolant passageway 320 in whichconcentric passageways 670 are disposed. Thus, because the areas of theconcentric passageways may vary, the time for fluid to traverse thedifferent concentric passageways may vary, and rapid temperature changesin cold reactor coolant passageway 320 are spread out over time.

Nuclear reactor system 5 may operate over any suitable time period suchas, for example, a period of years or of decades of continuousoperation. As nuclear reactor system operates over this period of yearsor decades, a size of gaseous zones 185, 185′, 185 a, 185 b, 280, and/or185 b will be caused to gradually shrink and substantially disappeartoward the end of the operation time period. Gaseous zones 185, 185′,185 a, 185 b, 280, and/or 185 b will be caused to shrink and eventuallysubstantially disappear because the amount of fissile content of thefuel in fuel tubes 135, 135′, 135 a, and/or 135 b will decrease overtime, and thus a higher density of moderator in control cavity arrays130, 130′, 130 a, and/or 130 b will be used to compensate for decreasedfissile content and to maintain a desired fission rate. Gaseous zones185, 185′, 185 a, 185 b, 280, and/or 185 b will also be caused to shrinkand eventually substantially disappear because neutron-absorbing fissionby-products will continuously accumulate over the period of operation ofnuclear reactor system 5. Accordingly, gaseous zones 185, 185′, 185 a,185 b, 280, and/or 185 b will also be caused to shrink and eventuallysubstantially disappear because of the increase in neutron-absorbingfission by-products over time, and thus a higher density of moderator incontrol cavity arrays 130, 130′, 130 a, and/or 130 b will also be usedto compensate for increased neutron capture and to maintain a desiredfission rate.

Over time, after gaseous zones 185, 185′, 185 a, 185 b, 280, and/or 185b have been caused to substantially disappear, the amount of fissilecontent of the fuel in fuel tubes 135, 135′, 135 a, and/or 135 b mayeventually become small enough and/or the amount of neutron-absorbingfission by-products produced in reactor 15 will eventually become largeenough so that reactor 15 becomes sub-critical and the fission rate innuclear reactor system 5 may become insignificant. Thus, reactor 15 willshut down. At this point, new fuel may be provided to reactor 15, orreactor 15 may be operated for brief periods after shut-down followingxenon decay.

Nuclear reactor system 5 may also be shut down, if desired, prior to theshut-down at the end of the operation time period described above.Nuclear reactor system may be intentionally shut down by reactor controlsubsystem 40. In the case of intentional shut-down, the operation ofreactor coolant subsystem 25 may be controlled to supply a relativelysmall amount or substantially no reactor coolant and/or moderatorcoolant to reactor 15. In this case, the moderator in control cavityarrays 130, 130′, 130 a, and/or 130 b will become very hot, causinggaseous zones 185, 185′, 185 a, 185 b, 280, and/or 185 b to expand tofill substantially all of control cavities 140, 140′, 140 a, and/or 140b. As described above, when gaseous zones 185, 185′, 185 a, 185 b, 280,and/or 185 b fill substantially all of control cavities 140, 140′, 140a, and/or 140 b, the average density of the moderator in control cavityarrays 130, 130′, 130 a, and/or 130 b decreases. This decrease inmoderator density increases the percentage of neutrons lost byabsorption at intermediate and high speeds (resonance capture), thusdecreasing the percentage of slow neutrons available to cause fission,which decreases the heating rate of reactor 15. Accordingly, if the flowof reactor coolant and moderator coolant to reactor 15 remains small orsubstantially stopped, gaseous zones 185, 185′, 185 a, 185 b, 280,and/or 185 b will continue to fill substantially all of control cavities140, 140′, 140 a, and/or 140 b, and reactor 15 will shut down. Similarto intentional shut-down, if reactor coolant subsystem 25 does notoperate properly and does not provide reactor coolant and/or moderatorcoolant to reactor 15, gaseous zones 185, 185′, 185 a, 185 b, 280,and/or 185 b will expand to fill substantially all of control cavities140, 140′, 140 a, and/or 140 b, and reactor 15 will eventually shut downon its own in the same manner as described above for intentionalshut-down.

The operation of auxiliary coolant subsystem 35 will now be described,beginning with a description of an exemplary operation of convectionloop subsystem 410.

Referring to FIG. 16, junctions 425 and 455 may be configured so that atsubstantially full coolant flow (full power operation) the pressure A inpassageway 430 and the pressure B in junction 455 oppose and balanceeach other so that there is substantially no fluid flow throughpassageways 430, 435, 440, and 445, merging portion 450, and junction455. If coolant pump 390 stops pumping cold reactor coolant through coldreactor coolant passageway 320, through reactor core 100, 100′, 100 a,and/or 100 b, and out hot reactor coolant passageway 325 to heatexchanger 20, then hot reactor coolant exiting reactor core 100, 100′,100 a, and/or 100 b may flow into passageway 430 of convection loopsubsystem 410 at junction 425. The hot reactor coolant flows downwardvia passageway 430, below an elevation of the top surface of reflectingpool 105. The hot reactor coolant then flows upward from passageway 430into passageway 435, and then toward containment structure 85 andpressure vessel 90 via the plurality of passageways 440. The hot reactorcoolant flows from the plurality of passageways 440 into thecorresponding plurality of passageways 445. The hot reactor coolantflows through the plurality of passageways 445, imparting heat by heatexchange to pressure vessel 90. The reactor coolant flows via theplurality of passageways 445 to a position near or below the bottom ofreactor core 100, 100′, 100 a, and/or 100 b. The reactor coolant thenflows into cold reactor coolant passageway 320 via junction 455. Reactorcoolant entering cold reactor coolant passageway 320 then enters reactorcore 100, 100′, 100 a, and/or 100 b. After exiting reactor core 100,100′, 100 a, and/or 100 b, some of the reactor coolant re-entersconvection loop subsystem 410 at junction 425.

Pressure A opposes and balances pressure B when pump 390 is circulatingcold moderator coolant at a rate corresponding to maximum poweroperation of the reactor so that very little coolant flows through theconvection loop at full power. At less than full power (which may be atmuch less than full reactor coolant flow or at substantially no reactorcoolant flow), a convection loop operates to circulate reactor coolantthrough convection loop subsystem 410. Thus, if desired, convection loopsubsystem 410 operates to circulate reactor coolant through reactor 15even when reactor coolant subsystem 25 is not operating. Convection loopsubsystem 410 and valves 460 and 465 may be autonomous systems thatoperate independently of controller 540 and of any electrical powersupply. For example, valves 460 and 465 may operate to isolate a flow ofreactor coolant within convection loop subsystem 410 in the case of aninterruption of flow of reactor coolant subsystem 25 or a leak in any ofthe coolant subsystem components outside containment structure 85. Valve460 operates to substantially block a flow of reactor coolant out ofreactor 15 via cold reactor coolant passageway 320 in any case when theexternal pressure is less than the pressure in cold reactor coolantpassageway 320 inside pressure vessel 90. Also, valve 465 operates tosubstantially block flow of reactor coolant out of reactor 15, when theamount of reactor coolant in reactor 15 is less than a desired thresholdamount. Thus, convection loop subsystem 410 operates to maintaincirculation of reactor coolant through reactor 15, independently of anoperation of reactor coolant subsystem 25, if desired.

Referring to FIGS. 17 and 18, an exemplary operation of auxiliary heatexchange subsystem 415 will now be described. When the temperature ofthe moderator within reflector zone 95 exceeds its normal operatingtemperature, pressure vessel 90 is also heated to about the sametemperature by conduction from the moderator and the moderator steam.The state-changing material housed within heat exchange member 470 isincreasingly heated. If heated beyond a threshold level, thestate-changing material disposed in heat exchange members 470 will becaused to change states (e.g., heated from a solid state into a liquidstate, or heated from a liquid state into a gaseous state), whichimproves the conductivity properties of the state-changing materialdisposed in heat exchange members 470. The state-changing material ofheat exchange member 470 will efficiently transfer heat away frompressure vessel 90 by convection or steam transfer, and toward anexterior of containment structure 85 (which may have low thermalconductivity).

The state-changing material of heat exchange member 475 is then heatedby heat transferred from heat exchange member 470. If heated beyond athreshold level, the state-changing material disposed in heat exchangemembers 475 will be caused to change states (e.g., heated from a solidstate into a liquid state, or heated from a liquid state into a gaseousstate), which improves the conductivity properties of the state-changingmaterial disposed in heat exchange members 475.

The state-changing material of heat exchange members 475 will then flowfrom heat exchange member 475 into heat exchange member 480. When heatexchange members 480 extend under a large area of terrain (e.g., fieldand/or parking lot), heat transferred by the state-changing materialdisposed and/or flowing in heat exchange members 480 will dissipate intothe adjacent terrain and ground surface. Also, when heat exchangemembers 480 are disposed at a slight angle upward from a substantiallyhorizontal plane, state-changing material disposed and/or flowing withinheat exchange member 480 increasingly dissipates heat as the distancefrom reactor 15 increases.

When cooled beyond the threshold level, the state-changing materialdisposed in heat exchange members 480 will be caused to change statesagain (e.g., cooled from a gaseous state into a liquid state, or cooledfrom a liquid state into a solid state). For example, if thestate-changing material disposed in heat exchange members 475 and 480 isH₂O, steam (H₂O) condenses into water (H₂O). When heat exchange members480 are disposed at a slight angle upward from a substantiallyhorizontal plane, the state-changing material, e.g., water (H₂O), willform steam bubbles in heat exchange members 475 that rise rapidly to thetop of heat exchange members 475 and then flow outward along the tops ofheat exchange members 480 until they condense into the colder water(H₂O) in heat exchange members 480 and flow due to gravity back towardreactor 15. As the state-changing material flows back through heatexchanging members 480 due to gravity toward reactor 15 and heatexchange members 475, the state-changing material again becomesincreasingly heated. If heated beyond a threshold level, thestate-changing material disposed in heat exchange members 475 will becaused to change states (e.g., heated from a liquid state into a gaseousstate, or heated from a solid state into a liquid state). Thestate-changing material may be iteratively heated and cooled, therebychanging back and forth between states in a cycle, and continuouslytransferring heat away from reactor 15 to be dissipated over the largearea of terrain (e.g., field and/or parking lot) under which heatexchange members 480 extend. It is contemplated that in addition tooperating within nuclear reactor system 5, auxiliary heat exchangesubsystem 415 may be used in conjunction with any suitable heat transferapplication in which heat is transferred away from a central source(e.g., any type of power plant, any type of heat-producing structuressuch as commercial buildings, military applications, residentialstructures and complexes, and/or sports complexes).

Referring to FIG. 19, an exemplary operation of auxiliary reactorshutdown subsystem 420 will now be described. During normal operation ofreactor 15, valve 487 may remain closed. When an influx ofneutron-absorbing material into reactor 15 is desired (e.g., when ashut-down of reactor 15 is desired), controller 540 controls valve 487to open to allow flow of pressurized neutron absorbing material frompressurized reservoir 485 into one or more passageways 490. Theneutron-absorbing material flows through one or more passageways 490,thereby flowing through reactor core 100, 100′, 100 a, and/or 100 b. Asthe neutron-absorbing material flows toward end portion 505, the steam(H₂O) previously disposed in passageway 490 becomes increasinglypressurized at closed end portion 505, which serves as a buffer andreduces the possibility of the flow of neutron absorbing materialbursting out of end portion 505 due to the force from the pressurizedflow from pressurized reservoir 485 into passageway 490. Due to thepresence of neutron-absorbing material in passageways 490, an increasedamount of neutrons are absorbed from reactor 15, which decreases thefission rate of reactor 15. Controller 540 controls pump 500 to pump theneutron-absorbing material from passageway 490 back to reservoir 485 viadrain passageway 495 when it is desired to restart the reactor. Whensubstantially no neutron-absorbing material is desired in passageway490, controller 540 controls valve 487 to substantially fully close, andcontrols pump 500 to evacuate neutron-absorbing material from passageway490 into pressurized reservoir 485. Pump 500 maintains pressurizedreservoir 485 in a pressurized state, and the above-described processmay be repeated as desired.

The disclosed nuclear reactor system may be used to make control of anuclear reactor easier. For example, reactor 15 may be constructed withno moving parts within containments structure 85. The disclosed controlmethod has a relatively large range (e.g., over 250 mk), which allowsthe use of fuels having widely differing reactivities, while achieving asubstantially maximum conversion ratio for each different fuel atsubstantially all points in the fuel life cycle. The disclosed nuclearreactor system also greatly increases the conversion ratio and thusincreases fuel life. Also, because of the relatively large range of thedisclosed control method, reactor 15 may use higher reactivity fuelssuch as, for example, low enriched uranium, MOX fuel, used light waterreactor fuel, and combinations of fuel which include thorium.

Because the disclosed control cavities react independently of each otherto control the local neutron flux, xenon waves may be naturallysuppressed, which increases efficiency of reactor 15. Also, the neutronflux across reactor core 100, 100′, 100 a, and/or 100 b is greatlyflattened, allowing a relatively higher total power output of nuclearreactor system 5. Also, fuel burnout across reactor core 100, 100′, 100a, and/or 100 b may be relatively even.

The disclosed nuclear reactor system may not have to use continuous orpartial refueling because the excess neutrons may be used to extend thelife of higher conversion ratio fresh fuel, instead of being used toless effectively extend the life of older fuel having a lower conversionratio. Because reactor 15 may use natural uranium for fuel, reactor 15may not utilize isotope (e.g., uranium) enrichment capability, thusdecreasing the possibility of nuclear proliferation. Because of the highconversion ratio of reactor 15, much of the power output is produced byfission of plutonium isotopes (mostly Pu239) produced from U238 inreactor 15, thus significantly increasing the total KWH of powerproduced per ton of mined uranium and significantly decreasing theamount of nuclear waste generated per KWH of power produced.

The disclosed control cavities may provide reactor 15 with a simplestructure for efficiently controlling nuclear reactor system 5. Thedisclosed control cavities may provide for a reduced temperaturedifference between reactor coolant and moderator, so that the heat lossfrom the hot coolant to the moderator is reduced, allowing higher outputcoolant temperatures and more efficient steam turbines. Also, thedisclosed control cavities may provide for a reduced pressure differenceacross reactor 15, allowing the coolant pressure tubes to be made withless structural material, which absorbs fewer neutrons and may increasethe conversion ratio of the fuel.

The disclosed fuel assemblies may provide inner fuel rods in thedisclosed fuel tubes that are relatively less shaded from thermalneutrons by outer fuel rods so that temperatures are relatively evenacross the fuel tubes, which allows the fuel tubes and fuel assembliesto contain more fuel rods and/or larger diameter fuel rods. Accordingly,the power output per reactor volume may be increased.

Auxiliary heat exchange system 415 may provide a method for efficientlytransferring heat from reactor 15, or from any other suitable heatsource. Auxiliary heat exchange system 415 provides an efficient heattransfer system that may operate without moving mechanical parts.

The disclosed nuclear reactor system may also provide for automaticallyand/or intentionally shutting down reactor 15 when desired. Thedisclosed reactor system may also provide methods for controlling anamount of steam that is delivered to turbine 45 via a bypass system,which may make control of power production more efficient.

It will be apparent to those skilled in the art that variousmodifications and variations can be made to the disclosed nuclearreactor system. Other embodiments will be apparent to those skilled inthe art from consideration of the specification and practice of thedisclosed method and apparatus. It is intended that the specificationand examples be considered as exemplary only, with a true scope beingindicated by the following claims and their equivalents.

What is claimed is:
 1. An apparatus for a nuclear reactor, comprising: acontainment structure, with the following being disposed in thecontainment structure: a reactor core that includes a fuel assembly, thefuel assembly including a plurality of fuel elements; a reflector zonethat surrounds the reactor core; neutron moderating material, wherein atleast some of the neutron moderating material is a fluid and the fluidneutron moderating material is disposed in both the reactor core and thereflector zone; a plurality of housings disposed adjacent to the fuelelements, each housing having a cavity and wherein a lower portion ofeach housing is open for movement of fluid neutron moderating materialinto and out of the cavity and an upper portion of each housing isclosed for movement of fluid neutron moderating material into or out ofthe upper portion of the cavity; and a plurality of cone assemblies thatencircle the fuel elements; wherein the fluid neutron moderatingmaterial moves from at least one of the plurality of housings to thereflector zone through the lower portion of at least one of theplurality of housings, and the fluid neutron moderating material movesfrom the reflector zone to at least one of the plurality of housingsthrough the lower portion of at least one of the plurality of housings.2. The apparatus of claim 1, wherein each cone assembly has an innercone assembly and an outer cone assembly.
 3. The apparatus of claim 2,wherein the inner cone assembly of each cone assembly encircles aportion of the fuel elements, and the outer cone assembly of each coneassembly encircles the inner cone assembly of each cone assembly.
 4. Theapparatus of claim 2, wherein the inner cone assembly of each coneassembly includes a cone having a height that is about twice a height ofeach of the housings.
 5. The apparatus of claim 4, wherein each conepasses through one of a plurality of apertures disposed at a top portionof one of the plurality of housings.
 6. The apparatus of claim 4,wherein a lower portion of a first cone of a first inner cone assemblyoverlaps with an upper portion of a second cone of a second inner coneassembly, the lower portion of the first cone encircling the upperportion of the second cone.
 7. The apparatus of claim 6, wherein apassage is formed between the lower portion of the first cone and theupper portion of the second cone.
 8. The apparatus of claim 2, whereinthe outer cone assembly of each cone assembly includes an interior coneand an exterior cone.
 9. The apparatus of claim 8, wherein the interiorcone of the outer cone assembly of each cone assembly encircles aportion of the inner cone assembly of each cone assembly.
 10. Theapparatus of claim 8, wherein the exterior cone of the outer coneassembly of each cone assembly encircles a portion of the interior coneof the outer cone assembly of each cone assembly.
 11. The apparatus ofclaim 8, wherein the interior cone of the outer cone assembly of eachcone assembly has a height that is slightly less than a height of eachof the housings.
 12. The apparatus of claim 8, wherein the exterior coneof the outer cone assembly of each cone assembly has a height that isless than a height of the interior cone of the outer cone assembly ofeach cone assembly.
 13. The apparatus of claim 8, wherein a cavity isformed between the interior cone and the exterior cone of the outer coneassembly of each cone assembly.
 14. The apparatus of claim 8, whereinthe inner cone assembly of each cone assembly includes a cone, apassageway being formed between the cone of the inner cone assembly ofeach cone assembly and the interior cone of the outer cone assembly ofeach cone assembly.
 15. The apparatus of claim 1, wherein at least someof the neutron moderating material is in a liquid state and at leastsome of the neutron moderating material is in a gaseous state in boththe reflector zone and in at least some of the cone assemblies.
 16. Theapparatus of claim 1, wherein the fluid neutron moderating materialdisposed in the cone assemblies is heavy water (D₂O).
 17. The apparatusof claim 1, wherein the fluid neutron moderating material disposed inthe cone assemblies is light water (H₂O).